Index Page Rotation
## Table of Contents
       Rotation
          Abstract
          Introduction
             Using this document
             References
             Notation
       CSPICE Functions
             Categories of functions
          Euler angle functions
             Constructing a matrix from Euler angles
             Finding Euler angles that represent a matrix
             Programming hazards
             Working with RA, Dec and Twist
          Quaternions
             Finding a quaternion that represents a matrix
             Finding the matrix represented by a quaternion
             q2m_c and m2q_c are approximate inverses of each other
             Multiplying quaternions
             Obtaining angular velocity from quaternions
          Rotating vectors and matrices
             A word of warning
             Rotating a vector about a coordinate axis
             Rotating a matrix about a coordinate axis
             Rotating a vector about an arbitrary axis
          Rotation axis and angle
             Constructing a matrix from a rotation axis and angle
             Finding the axis and angle of a rotation matrix
             axisar_c and raxisa_c are approximate inverses
             Using raxisa_c and axisar_c
             Constructing a coordinate axis rotation matrix
          Rotation derivatives
             Differentiating rotations
             State transformations
          Validating a rotation matrix
       Tutorial introduction to rotations
          A comment of the heuristic variety
          Definition of ``rotation''
             Definition 1
             Definition 2
             Definition 3
             Uses of the definitions
          Definition of ``rotation'' and ``orthogonal'' matrix
          Rotations preserve inner products
          Inverses of rotation matrices
          Composition of rotations
          Coordinate transformations
          Rotation of vectors in the plane
          A canonical representation for rotations
          Rotation axis and angle
          Time-dependent coordinate transformations
          Euler angles
          Quaternions
          Quaternion arithmetic
             Definitions
             Basic properties of multiplication
             Deducing the multiplication formula
             Composing rotations using quaternions
       Mathematical road map
          Rotation of a vector about an axis
          Formation of a rotation matrix from axis and angle
          Finding the axis and angle of a rotation matrix
          Formation of a rotation matrix from a quaternion
          Equivalence of rotation definitions
             An algebraic approach
             A geometric approach
          Quaternion multiplication
             Assertion 1
             Assertion 2
          Recovery of Euler angles from a rotation matrix
             Euler angle recovery: a-b-a case
             Euler angle recovery: a-b-c case
       Appendix A: Document Revision History
             May 27, 2010
             November 17, 2005
             January 10, 2005
             February 2, 2004
             December 2, 2002
             April 26, 1999
Top # Rotation Last revised on 2010 MAY 27 by E. D. Wright. Top ## Abstract The SPICE rotation routines manipulate and convert between different representations of rotation transformations: matrices, quaternions, Euler angles, and axis-angle pairs. Top ## Introduction This document covers the CSPICE routines that deal with rotations and the mathematical ideas behind the routines. There are three chapters: `--` CSPICE routines `` The ``CSPICE routines'' chapter tells you what routines are available, what they do, and how to call them. `--` Tutorial introduction to rotations `` If rotations are new to you, you'll profit most by reading the ``tutorial'' chapter first. This chapter lists most of the facts about rotations used in the CSPICE code. The emphasis is on building intuition about rotations; proofs of any noticeable difficulty or length are deferred to the ``Mathematical Road Map'' chapter. `--` Mathematical road map `` This chapter contains detailed explanations of a number of the mathematical ideas used in the CSPICE rotation routines. And as we've said, proofs of some of assertions made in the tutorial chapter are stowed here. Top ### Using this document For many readers, the first chapter will be the only one of interest. The mechanics of using the rotation routines in your code are covered here. The rest of the document covers the ideas behind the code. This material is meant to be used as a reference rather than to be read from start to finish; the topics are ordered loosely according to logical dependence, but there is no narrative progression from section to section. The purpose of the tutorial and ``road map'' chapters is to make it easier to be certain that you're using the code correctly. In our experience, thinking about this category of code only in terms of ``inputs'' and ``outputs'' is a tricky and error-prone approach; really understanding the mathematics helps you to verify that you're putting the pieces together in ways that make sense. Because some of the ideas required to understand the code seem to exist as lore and are rarely written down, we've collected them here for your convenience. Top ### References `1.` For CSPICE routines dealing with inertial reference frames: SPK ``required reading.'' (spk.req) `2.` For CSPICE routines dealing with body-fixed reference frames: KERNEL ``required reading.'' (kernel.req) `3.` For linear algebra: ``Calculus, Vol. II.'' Tom M. Apostol. Wiley and Sons, 1969. `` Also, ``Elementary Linear Algebra.'' Howard Anton. Wiley and Sons, 1977. `4.` NAIF document number 179.0, ``Rotations and Their Habits,'' by Dr. William Taber. `5.` NAIF document number 192.0, ``Memo to: Quaternion Seekers,'' by Allen Klumpp. Top ### Notation Here are the symbols used in this document, and their definitions:
        Symbol                      Meaning
       ---------          ----------------------------------

          E3              Three-dimensional Euclidean space.

          E2              Two-dimensional Euclidean space.

       < u, v >           Inner product of vectors u and v.

            T
          M               Transpose of the matrix M.

           -1
          M               Inverse of the matrix M.

           -1
          f               Inverse of the function f.

        u x v             Cross product of vectors u and v.

         M v              Product of matrix M and vector v.

         M N              Product of matrix M and matrix N.

       Trace(M)           Sum of elements on the main diagonal of M.

         [w]              Matrix that rotates a coordinate system by
            i             w radians about the ith coordinate axis
                          (and rotates vectors by -w radians about the
                          same axis).  We also use this notation to refer
                          to the linear transformation corresponding to
                          this matrix.
There are only three types of rotation matrices representing rotations about coordinate axes:
                +-                        -+
                |     1       0        0   |
       [w]   =  |     0    cos(w)   sin(w) |
          1     |     0   -sin(w)   cos(w) |
                +-                        -+

                +-                        -+
                |  cos(w)     0    -sin(w) |
       [w]   =  |     0       1        0   |
          2     |  sin(w)     0     cos(w) |
                +-                        -+

                +-                        -+
                |  cos(w)  sin(w)      0   |
       [w]   =  | -sin(w)  cos(w)      0   |
          3     |     0       0        1   |
                +-                        -+
The composition of rotations
       [w1]   [w2]   [w3]
           a      b      c
is sometimes referred to as a ``a-b-c'' rotation. For example, we may talk about a ``3-1-3'' rotation. About angles: all angles in this document are measured in radians. About directions: the ``right hand rule'' is in effect at all times in this document, so counterclockwise rotations about an axis have positive measure. Top # CSPICE Functions This chapter describes the CSPICE functions that deal with rotations. The chapter lists the CSPICE rotation functions and discusses each function. The CSPICE functions that deal with general rotations are: axisar_c ( Axis and angle to rotation ) drotat_c ( Derivative of a rotation matrix ) eul2m_c ( Euler angles to matrix ) eul2xf_c ( Euler angles and derivative to transformation ) invstm_c ( Inverse of state transformation matrix ) isrot_c ( Is it a rotation matrix? ) m2eul_c ( Matrix to Euler angles ) m2q_c ( Matrix to quaternion ) pxform_c ( Position transformation matrix ) q2m_c ( Quaternion to matrix ) qdq2av_c ( Quaternion and derivative to angular velocity ) qxq_c ( Quaternion times quaternion ) raxisa_c ( Rotation axis and angle ) rav2xf_c ( Rotation and angular velocity to transform ) rotate_c ( Generate a rotation matrix ) rotmat_c ( Rotate a matrix about a coordinate axis ) rotvec_c ( Rotate a vector about a coordinate axis ) sxform_c ( State transformation matrix ) tipbod_c ( Transformation, inertial position to bodyfixed ) tisbod_c ( Transformation, inertial state to bodyfixed ) vrotv_c ( Rotate a vector about an arbitrary axis ) xf2eul_c ( State transformation to Euler angles ) xf2rav_c ( Transform to rotation and angular velocity) Additional CSPICE functions that deal with rotations between specific coordinate systems are documented in the FRAMES required reading and in the header of the CSPICE function sxform_c. Top ### Categories of functions The discussions of the functions are categorized according to the type of problem that the functions solve. This chapter contains one section for each category. The categories are: `--` Euler angles `--` Quaternions `--` Rotating vectors and matrices `--` Rotation axis and angle `--` Rotation derivatives `--` Validating rotation matrices The rotation functions constitute a ``family'' of functions insofar as they deal with related problems, but they do not constitute a ``system.'' So, there is no logical interdependence between the discussions of functions in different categories. Top ## Euler angle functions The CSPICE Euler angle functions are: eul2m_c ( Euler angles to matrix ) m2eul_c ( Matrix to Euler angles ) eul2m_c and m2eul_c provide a convenient way to solve problems such as converting between C-matrices and RA, Dec, and Twist. These functions are inverses of each other, roughly speaking. Top ### Constructing a matrix from Euler angles The function eul2m_c constructs the rotation matrix defined by three Euler angles ang[2], ang[1], ang[0], and three coordinate axes indexed by the integers i[2], i[1], i[0]. The call
       eul2m_c ( ang[2], ang[1], ang[0],
                 i[2],   i[1],   i[0],   m );
returns the matrix `m', where
       m   =   [ang[2]]       [ang[1]]        [ang[0]]    .
                       i[2]           i[1]            i[0]
The indices i[2], i[1], i[0] must belong to the set
       {1, 2, 3}.
Top ### Finding Euler angles that represent a matrix Given a rotation matrix `m' and three coordinate axes indexed by the integers i[2], i[1], i[0], the function m2eul_c finds angles ang[2], ang[1], ang[0] such that
       m   =   [ang[2]]       [ang[1]]        [ang[0]]    .
                       i[2]           i[1]            i[0]
The call
       m2eul_c ( m, i[2], i[1], i[0], ang+2, ang+1, ang );
returns the desired angles. m2eul_c restricts the ranges of the output angles so as to guarantee that the Euler angle representation is unique. The output angles ang[2] and ang[0] are always in the range (-pi,pi]. The range of ang[1] is determined by the set of rotation axes. When i[2] equals i[0], ang[1] is in the range [0, pi]. Otherwise, ang[1] is in the range [-pi/2, pi/2]. These ranges make unique determinations of Euler angles possible, except in degenerate cases. In cases where the Euler angles are not uniquely determined, eul2m_c sets the first angle (called ang[2] above) to zero. The other two angles are then uniquely determined. Again, the indices i[2], i[1], i[0] are members of
       {1, 2, 3}.
There is a restriction on the allowed set of coordinate axes: i[1] must not equal i[2] or i[0]. If this constraint is not met, the desired representation of `m' by Euler angles may not exist; m2eul_c signals an error in this case. Top ### Programming hazards There are several pitfalls associated with converting matrices to Euler angles. First, any mapping from matrices to Euler angles has singularities. These come in two flavors: some matrices don't map to a unique set of Euler angles, and some matrices have the property that a small change in the matrix can result in a large change in the corresponding Euler angles. The first category of singularity occurs with matrices that represent rotations about the first or third axis in the sequence of rotation axes (for example, axis 3 for a 2-1-3 rotation). In practical terms, if eul2m_c encounters one of these special matrices, eul2m_c must choose the Euler angles. Immediately the possibility arises that eul2m_c will disagree with any other code performing the same task. The second kind of singularity occurs when any of the Euler angles corresponding to a matrix is at one of the endpoints of its range, for example, when the first angle has the value pi. If the matrix is perturbed slightly, the first angle may jump from pi to a value close to -pi. Again, two different pieces of code may give different results in such a case, merely because of round-off error. Euler angles near the limits of their ranges should be regarded with suspicion. The existence of singularities in the matrix-to-Euler angle mapping prevents eul2m_c and m2eul_c from being exact inverses: most of the time, the code fragment
       eul2m_c (    ang[2],  ang[1],  ang[0],
                    axis[2], axis[1], axis[0], m );

       m2eul_c ( m, axis[2], axis[1], axis[0],
                    ang+2,   ang+1,   ang        );
leaves the angles ang[2], ang[1], ang[0] unchanged, except for round-off error, but in some cases, the angles may change drastically. If we reverse the order of the function calls in the last code fragment, the matrix `m' should be preserved, except for errors due to loss of precision. The loss of precision can be considerable, though, for matrices whose entries are nearly those of any degenerate case matrix. For more details on this topic, consult the ``Mathematical road map'' section. Top ### Working with RA, Dec and Twist The Euler angle routines could be used for conversion between ``RA, Dec, and Twist'' and a ``C-matrix.'' Most projects, including Voyager and Cassini define the relationship as:
       c  =  [ Twist ]   [ pi/2 - Dec ]   [ pi/2 + RA ]
                      3                1               3
so the code fragments
       eul2m_c ( twist,   halfpi_c() - dec,   halfpi_c() + ra,
                 3,       1,                  3,                 c  );
and
       m2eul_c ( c, 3, 1, 3, ang+2, ang+1, ang );

       twist =  ang[2];
       dec   =  halfpi_c() - ang[1];
       ra    =  ang[0]     - halfpi_c();
carry out the conversion from RA, Dec, and Twist to a C matrix, and back. Note that definitions of ``RA, Dec, and Twist'' vary: on the Galileo project, the C matrix is related to the angles ``RA, Dec, and Twist'' by the equation
       C  =  [ Twist ]   [ pi/2 - Dec ]    [ RA ] .
                      3                2         3
Top ## Quaternions The CSPICE quaternion routines are: m2q_c ( Matrix to quaternion ) q2m_c ( Quaternion to matrix ) qdq2av_c ( Quaternion and derivative to angular velocity ) qxq_c ( Quaternion times quaternion ) Quaternions are used in CSPICE as a compact representation for rotations. They may be used to compose rotations more efficiently than can be done with matrix multiplication. Top ### Finding a quaternion that represents a matrix The routine m2q_c produces a quaternion that represents a specified rotation matrix. The code fragment
       m2q_c ( m, q );
returns a unit quaternion `q' that represents the rotation matrix `m'. If you really want to know about it, the elements of the quaternion are defined as follows: Let the unit vector `a' be a choice of rotation axis for `m', and let `angle' be the rotation angle, where `angle' is in the interval
       [0, pi]
Then the elements of the unit quaternion `q' returned by m2q_c are
       q[0] = cos( angle/2 )

       q[1] = sin( angle/2 ) * a[0]
       q[2] = sin( angle/2 ) * a[1]
       q[3] = sin( angle/2 ) * a[2]
m2q_c considers the rotation angle of `m' to lie in [0, pi]. Therefore, half the rotation angle lies in [0, pi/2], so Q(0) is always in [0, 1]. For a given rotation matrix `m', the corresponding quaternion is uniquely determined except if the rotation angle is pi. Top ### Finding the matrix represented by a quaternion The routine q2m_c inverts the transformation performed by m2q_c. The following call finds the rotation matrix `m' represented by the unit quaternion `q':
       q2m_c ( q, m );
Top ### q2m_c and m2q_c are approximate inverses of each other The calls
       m2q_c ( m, q );
       q2m_c ( q, m );
always preserve `m', except for round-off error. However, since there are two quaternions that represent each rotation, the sequence of calls
       q2m_c ( q, m );
       m2q_c ( m, q );
do not necessarily preserve `q'. Top ### Multiplying quaternions Two quaternions `q1', `q2' may be multiplied by calling qxq_c:
       qxq_c ( q1, q2, qout );
The resulting product `qout' is computed using the multiplication formula given in the section ``Quaternion Arithmetic'' below. `qout' represents the rotation formed by composing the rotations represented by `q1' and `q2'. Top ### Obtaining angular velocity from quaternions Given a quaternion `q' and its derivative with respect to time `dq', the angular velocity of the reference frame represented by `q' may be found by calling qdq2av_c:
       qdq2av_c ( q, dq, av );
The resulting angular velocity vector `av' has units of radians/T, where 1/T is the time unit associated with `dq'. Top ## Rotating vectors and matrices The CSPICE routines that ``rotate'' vectors and matrices are: rotvec_c ( Rotate vector ) rotmat_c ( Rotate matrix ) vrotv_c ( Rotate a vector about an axis ) This set of routines are frequently used as utilities from which more complicated routines may be constructed. For example, the routine eul2m_c constructs a rotation matrix from a sequence of three rotations about specified coordinate axis, so there is no need to call rotmat_c directly to accomplish this. Top ### A word of warning Some care is needed when dealing with signs of rotation angles: a rotation of a vector by an angle `theta' can be viewed as rotating the coordinate system by -`theta'. We try to avoid confusion here by referring to routines as ``coordinate system rotations'' or ``vector rotations,'' depending on whether a positive rotation angle corresponds to rotating the coordinate system by a positive angle, or to rotating a vector by a positive angle. The same criterion applies to matrix rotations. According to this classification, rotvec_c and rotmat_c perform coordinate rotations, and vrotv_c performs a vector rotation. Top ### Rotating a vector about a coordinate axis To apply the rotation
       [angle]
              i
to a vector, use rotvec_c. The following code fragment applies
       [ angle ]
                3
to the vector `v', yielding `vout'.
       rotvec_c ( v, angle, 3, vout );
The components of `vout' are the coordinates of the vector `v' in a system rotated by `angle' radians about the third coordinate axis. We can also regard `vout' as `v', rotated by
       -angle
radians about the third coordinate axis. Top ### Rotating a matrix about a coordinate axis We can apply the same rotation
       [angle]
              i
to a matrix using rotmat_c, as follows:
       rotmat_c ( m, angle, 3, mout );
After this function call, `mout' is equal to
       [ angle ]  * m
                3
Top ### Rotating a vector about an arbitrary axis We can rotate a vector about an arbitrary axis using vrotv_c. The code fragment
       vrotv_c ( v, axis, angle, vout );
rotates the vector `v' about the vector `axis' by `angle' radians, yielding `vout'. Top ## Rotation axis and angle There are three CSPICE routines that deal with rotation axes and angles: axisar_c ( Axis and angle to rotation ) raxisa_c ( Rotation axis and angle ) rotate_c ( Generate a rotation matrix ) Like the routines that rotate vectors and matrices, these routines are frequently used as building blocks for more sophisticated routines. Top ### Constructing a matrix from a rotation axis and angle To generate a matrix that rotates vectors by a specified angle about an arbitrary axis, use axisar_c. If `axis' is the axis vector and `angle' is the rotation angle, the code fragment
       axisar_c ( axis, angle, m );
produces `m', the desired rotation matrix. What if we want generate a coordinate system rotation about an arbitrary axis, as opposed to a coordinate axis? We can use axisar_c for this. Let `axis' be the coordinate system rotation axis and `angle' be the rotation angle; then the code fragment
       axisar_c ( axis, -angle, m );
produces the desired coordinate system rotation matrix. Note that the input angle is the NEGATIVE of that associated with a vector rotation. axisar_c is designed this way for compatibility with raxisa_c, which is an inverse routine for axisar_c. Top ### Finding the axis and angle of a rotation matrix To find the rotation axis and angle of a rotation matrix `m', use raxisa_c:
       raxisa_c ( m, axis, &angle );
`axis' and `angle' have the property that for any vector `v',
       m v
yields `v', rotated by `angle' radians about the vector `axis'. If `m' is viewed as a coordinate transformation, we can say that `m' rotates the initial coordinate system by
       - angle
radians about `axis'. Top ### axisar_c and raxisa_c are approximate inverses The code fragment
       raxisa_c ( m,      axis,   &angle );
       axisar_c ( axist,  angle,  m      );
leaves `m' unchanged, except for round-off error. The code fragment
       axisar_c ( axist,  angle,  m      );
       raxisa_c ( m,      axis,   &angle );
usually leaves `axis' and `angle' unchanged, except for round-off error, provided that two conditions are met: `--` `angle' is in the range (0,pi) `--` `axis' is a unit vector. If `angle' is near zero or pi, loss of precision may preclude recovery of `axis'. Top ### Using raxisa_c and axisar_c raxisa_c and axisar_c can be used to perform linear interpolation between two rotation matrices. Here's a code fragment illustrating the procedure:
          /*
          Let r(t) be a time-varying rotation matrix; r could be
          a C-matrix describing the orientation of a spacecraft
          structure.  Given two points in time t1 and t2 at which
          r(t) is known, and given a third time t3, where

             t1  <  t3  <  t2,

          we can estimate r(t3) by linear interpolation.  In other
          words, we approximate the motion of r by pretending that
          r rotates about a fixed axis at a uniform angular rate
          during the time interval [t1, t2].  More specifically, we
          assume that each column vector of r rotates in this
          fashion.  This procedure will not work if r rotates through
          an angle of pi radians or more during the time interval
          [t1, t2]; an aliasing effect would occur in that case.

          If we let

             r1 = r(t1)
             r2 = r(t2), and

                         -1
             q  = r2 * r1  ,

          then the rotation axis and angle of q define the rotation
          that each column of r(t) undergoes from time t1 to time
          t2.  Since r(t) is orthogonal, we can find q using the
          transpose of r1.  We find the rotation axis and angle via
          raxisa_c.
          */

          mxmt_c    ( r2, r1,    q      );
          raxisa_c  ( q,  axis,  &angle );

          /*
          Find the fraction of the total rotation angle that r
          rotates through in the time interval [t1, t3].
          */
          frac = ( t3 - t1 )  /  ( t2 - t1 );

          /*
          Finally, find the rotation delta that r(t) undergoes
          during the time interval [t1, t3], and apply that rotation
          to r1, yielding r(t3), which we'll call r3.
          */
          axisar_c ( axis,  frac * angle, delta );
          mxm_c    ( delta, r1,           r3    );
Top ### Constructing a coordinate axis rotation matrix The routine rotate_c generates the rotation matrix
       [ angle ] ,
                i
which corresponds to a rotation about a coordinate axis. This is a special case of the problem solved by axisar_c. Note however that the matrix produced by rotate_c is the inverse of that produced by axisar_c, if both routines are provided with the same input angle, and axisar_c is given the ith coordinate basis vector as the rotation axis. The call
       rotate_c ( angle, i, m );
produces `m', the desired matrix. Top ## Rotation derivatives The CSPICE routines that deal with derivatives of rotations are: drotat_c ( Derivative of a rotation matrix ) invstm_c ( Inverse of state transformation matrix ) tisbod_c ( Transformation, inertial state to bodyfixed ) The rotation derivative routines are utilities that simplify finding derivatives of time-varying coordinate transformations. In particular, these routines are used to transform state vectors between non-inertial reference frames. Top ### Differentiating rotations The routine drotat_c gives the derivative of a coordinate axis rotation with respect to the rotation angle. For example, the transformation
       [ angle ]
                1
which has the matrix representation
       +-                             -+
       |  1         0           0      |
       |  0    cos(angle)  sin(angle)  |
       |  0   -sin(angle)  cos(angle)  |
       +-                             -+
yields, when differentiated with respect to `angle', the matrix
       +-                             -+
       |  0         0           0      |
       |  0   -sin(angle)  cos(angle)  |
       |  0   -cos(angle) -sin(angle)  |
       +-                             -+
The routine drotat_c is useful for differentiating rotations that are defined by time-varying Euler angles. For example, if the rotation `r' is defined by
       r = [ Twist ]    [ pi/2 - Dec ]    [ pi/2 + RA ]
                    3                 1                3
where RA, Dec, and Twist are time-dependent, then if we make the abbreviations
       A(Twist) = [ Twist ]
                           3

       B(Dec)   = [ pi/2 - Dec ]
                                1

       C(RA)    = [ pi/2 + RA ]
                               3
we can write
       d(r)            d(A)     d(Twist)
       ----  =       -------- * --------       *     B     *      C
        dt           d(Twist)      dt

                                         d(B)    - d(Dec)
                 +       A    *         ------ * --------  *      C
                                        d(Dec)      dt

                                                     d(C)     d(RA)
                 +       A    *        B       *     ----- * -------
                                                     d(RA)      dt
The derivatives of A, B, and C can be found using drotat_c. Top ### State transformations Transforming state vectors between inertial and non-inertial coordinates requires the derivative of the rotation that relates the two frames: Let
       p (t)
        I
be a position vector referenced to an inertial frame ``I,'' and let
       p (t)
        N
be the equivalent position vector referenced to a non-inertial frame ``N.'' If r(t) is the transformation from frame I to N at time t, then the two vectors are related as follows:
       p (t)  =  r(t) p (t)
        N              I
Therefore, the derivatives of the position vectors satisfy
       d [ p (t) ]               d [ p (t) ]
            N                         I              d [ r(t) ]
       -----------   =   r(t) *  -----------    +    ----------  *  p (t)
           dt                        dt                  dt          I
It's well to note that although `r'(t) may vary slowly, the second term in the above equation is not necessarily insignificant. For example, if `r'(t) describes a transformation between an inertial frame and a body-centered frame that uses a body-center-to-Sun vector to define one of its coordinate axes, then for any point that is fixed on this axis, the two addends above have equal and opposite magnitude. In particular, if the fixed point is the location of the Sun, the magnitude of the second addend is (ignoring the velocity of the Sun with respect to the inertial frame) that of the inertially referenced velocity of the body used to define the body-centered frame. CSPICE provides routines to transform states between inertial frames and body-fixed planetocentric frames. The routine tisbod_c returns the 6x6 transformation matrix required to transform inertially referenced state vectors to body-fixed planetocentric coordinates. If `ref' is the name of the inertial frame of interest, `body' is the NAIF integer code of a body defining a body-fixed planetocentric frame, and `et' is ephemeris time used to define the body-fixed frame, then the call
       tisbod_c ( ref, body, et, tsipm );
returns `tsipm', the desired 6x6 state transformation matrix. A state vector `s' can be transformed to the body-fixed state vector `sbfixd' by the function call
       mxvg_c ( tsipm, s, 6, 6, sbfixd );
Since the inverse of a state transformation matrix is not simply its transpose, CSPICE provides the utility routine invstm_c to perform the inversion. If `m' is a state transformation matrix, the inverse matrix `minv' can be obtained via the function call
       invstm_c ( m, minv );
Top ## Validating a rotation matrix isrot_c is a logical function that indicates whether a matrix is a valid rotation matrix. The criteria for validity are: `--` The columns of the matrix are unit vectors, within a specified tolerance. `--` The determinant of the matrix formed by unitizing the columns of the input matrix is 1, within a specified tolerance. This criterion ensures that the columns of the matrix are nearly orthogonal, and that they form a right-handed basis. We might use isrot_c as follows:
          /*
          Set values for the column norm and determinant tolerances
          ntol and dtol:
          */

          ntol = 1.e-7;
          dtol = 1.e-7;

          if ( ! isrot_c ( m, ntol, dtol )   )
          {
             [perform error handling]
          }
          else
          {
             m2q_c ( m, q );
                  .
                  .
                  .
          }
Top # Tutorial introduction to rotations This tutorial is intended to bridge the gap between knowing linear algebra and understanding rotations. If you haven't reached the gap yet, consult reference [2], or any reasonable textbook on the subject. In this section, we make some assertions that we don't prove. Our goal is to supply you with the most important information first, and fill in the details later. Proofs are supplied only when they're instructive and not too distracting. The longer or more difficult proofs are deferred to the ``Mathematical road map'' chapter. Top ## A comment of the heuristic variety If you're going to read the rest of this tutorial, you're going to see a lot of definitions, symbol manipulation, and proofs. This information may be more accessible if you have some kind of reasonable mental model of rotations; then you can test our claims against your model. We offer the following model: Take a soccer ball, put two fingers on diametrically opposed points on the ball, and rotate the ball through some angle, keeping your fingers in place. What you use to rotate the ball is up to you. Well, that's it. That's the effect of a rotation on a soccer ball. Now you're equipped to answer some questions about rotations. Do rotations preserve inner products of vectors? That is, is it true that for vectors u and v, and a rotation R,
       < R u,  R v >  =  < u, v > ?
Well, presume that your soccer ball is centered at the origin, and mark the ball where u and v, or extensions of them, intercept the surface (perhaps you could hold a marker pen between your teeth). Does rotating the ball change the angular separation of the marks? No. So rotations preserve angular separation. Does rotating the ball change the norm of u or of v? No. So rotations preserve both angular separation and norms, and hence inner products. Do rotations preserve cross products? For vectors u and v, is it true that
       ( R u )  x  ( R v )  =  R ( u x v )?
Mark the intercepts of u, v, and u x v on the soccer ball. After you rotate the ball, does the intercept mark of u x v still lie at the right place, relative to the u and v intercept marks? Yes. Since we already know that rotations preserve norms, we can conclude that they preserve cross products as well. The soccer ball model shows that rotations preserve geometrical relationships between vectors. Top ## Definition of ``rotation'' Actually, we present three definitions of the term ``rotation.'' What for? Having more than one way of knowing that a mapping is a rotation makes it easier to check whether any particular mapping is a rotation or not. Some properties of rotations are easier to derive from one definition than from another. Top ### Definition 1 A ``rotation'' R is a linear transformation defined on E3 that has the following properties: `--` R preserves norms: if v is a vector, then
       || R(v) ||  =  ||v||
`--` R preserves cross products: if a and b are vectors, then
       R ( a x b )  =  ( R a )  x  ( R b ).
Top ### Definition 2 A ``rotation' R is a mapping defined on E3 that satisfies definition (1), and also has the property: `--` R keeps some vector (called the rotation axis) fixed. That is, if n is the rotation axis, then
       R(n) = n.
`` Since R is linear, the entire line containing n is fixed. Top ### Definition 3 A rotation R is a linear mapping defined on E3 that has the following properties: `--` R preserves distances on the unit sphere. `--` R keeps exactly two points on the unit sphere fixed, or else R is the identity. `` This property rules out the possibility that R is a ``reflection.'' Top ### Uses of the definitions Definition (1) is useful for checking that a mapping is a rotation, because there's not much to check. Definition (2) obviously implies definition (1). Less obviously, definition (1) implies definition (2). This had better be true if definition (1) is valid, since we expect rotations to have rotation axes. In the ``Mathematical road map'' chapter, we prove that the two definitions are equivalent. Definition (3) is a mathematical paraphrase of our soccer ball model of rotations. Top ## Definition of ``rotation'' and ``orthogonal'' matrix A ``rotation matrix'' M is a 3 by 3 matrix whose columns form an orthonormal set, and whose third column is the cross product of the first two. Given a rotation R and an orthonormal basis B, the matrix representation of R relative to B is a rotation matrix. Any matrix whose columns form an orthonormal set is called an ``orthogonal'' matrix. Top ## Rotations preserve inner products This section is for those who do not feel comfortable with soccer ball arguments. Our definition of ``rotation'' says that rotations preserve norms of vectors. That is, if R is a rotation and v is a vector, then
       || R(v) ||  =  || v ||.
Preserving norms also implies the seemingly stronger property of preserving inner products: if R preserves norms and u, v are vectors, then
                          2               2
       ||  R ( u - v )  ||  =  || u - v ||

                            =  < u - v,  u - v >

                                      2                        2
                            =  || u ||  - 2 < u, v >  + || v ||,
and also
                          2
       ||  R ( u - v )  ||  =  < R ( u - v ),  R ( u - v ) >

                            =  < R(u) - R(v),  R(u) - R(v) >

                                         2               2
                            =  || R(u) ||   +  || R(v) ||

                                           -  2 < R u, R v >

                                      2             2
                            =  || u ||   +   || v ||

                                           -  2 < R u, R v >
so
       < R(u), R(v) >       =   < u, v >.
So rotations really do preserve inner products. In particular, for any orthonormal basis, the images of the basis vectors under a rotation are also an orthonormal set. Then rotation matrices, expressed relative to an orthonormal basis, are in fact orthogonal, as claimed. Top ## Inverses of rotation matrices We've seen that the columns of a rotation matrix R form an orthonormal set. Since the (i,j) entry of
        T
       R  R
is the inner product of the ith column of R and the jth column of R, all entries of the product are zero except for those on the main diagonal, and the entries on the main diagonal are all 1. So
        T
       R  R  =  I.
If A and B are square matrices with real or complex entries, it's a fact that if
       A B = I
then
       B A = I.
We won't prove this (the ``Nullity and Rank'' theorem is useful, if you wish to do so). But this result implies that
          T
       R R  = I,
given the previous result. This shows that the rows of R form an orthonormal set as well, and that the transpose of R is also a rotation matrix. Top ## Composition of rotations If we multiply a sequence of rotation matrices, is the result a rotation matrix? Equivalently, if we compose a sequence of rotations, is the resulting mapping a rotation? What does our soccer ball model say? We can rotate the ball as many times as we like, changing the rotation axis each time, without changing the distance of any surface point from the center, so norms are preserved. Similarly, after marking the intercepts of u, v, and u x v on the surface, we can perform any sequence of rotations without changing the position of the u x v intercept mark relative to those of u and v. So cross products are preserved. That's all we need to verify that the composition of a sequence of rotations is a rotation. It follows that the product of a sequence of rotation matrices is a rotation matrix. If you don't agree that that's all we need, we can present the same argument using the usual symbols: Suppose R1 and R2 are rotation mappings, and for any vector v,
       R3(v) = R2 ( R1(v) ).
Then for any vector v, we have
       || R3(v) ||  =  || R2 ( R1 v ) ||

                    =  || R1( v ) ||

                    =  || v ||.
So R3 preserves norms. If u and v are vectors, then
       R3 ( u x v ) =  R2 ( R1 ( u x v )  )

                    =  R2 ( R1(u)  x  R1(v) )

                    =  (  R2 ( R1(u) )   x   R2 ( R1(v) )  )

                    =  R3(u)  x  R3(v),
so R3 preserves cross products. We've used only the definition of R3 and the fact that R2 and R1 preserve cross products in this proof. We conclude that R3 is a rotation. We can extend the result to the product of a finite number of rotations by mathematical induction; the argument we've made is almost identical to the induction step. Top ## Coordinate transformations Change-of-basis transformations between right-handed, orthonormal bases are rotations. You can verify this using our first definition of rotations. In particular, the inertial coordinate system transformations available in CSPICE are all rotations. How do we transform a vector v from one coordinate system to another? This result really belongs to linear algebra, but we'll state it here because it seems to come up a lot. Given two vector space bases,
       B1 = { e1, e2, e3 },   B2 = { u1, u2, u3 },
and a vector v that has components ( v1, v2, v3 ) relative to B1, we wish to express v relative to B2. We can say that
       v  =  x1 u1 +  x2 u2  +  x3 u3,
where the x's are unknowns. Let M be the matrix whose columns are u1, u2, and u3, represented relative to basis B1. M represents the linear transformation T defined by
       T  (e1) = u1, T(e2) = u2, T(e3) = u3.
Then since
        -1         -1
       T  (v)  =  T  ( x1 u1 +  x2 u2  +  x3 u3 )

               =     ( x1 e1 +  x2 e2  +  x3 e3 ),
we see that
        -1
       M  v  = ( x1, x2, x3 ).
So we've found the components of v, relative to basis B2. In the case where B1 and B2 are orthonormal bases, the matrix M is orthogonal. So we have
        T
       M  v  = ( x1, x2, x3 ).
Conversely, if M is the matrix that transforms vectors from orthonormal basis B1 to orthonormal basis B2, then the rows of M are the basis vectors of B2. For example, if M is the matrix that transforms vectors from J2000 coordinates to body equator and prime meridian coordinates, then the first row is the vector, expressed in J2000 coordinates, that points from the body center to the intersection of the prime meridian and body equator. The third row is the vector, expressed in J2000 coordinates, that points from the body center toward the body's north pole. Top ## Rotation of vectors in the plane How do we rotate a two-dimensional vector v by theta radians? Trivial as this problem may seem, it's probably worth your while to get a firm grip on its solution. When you've understood it, you've almost understood three-dimensional rotations. We can assume that v is a unit vector; since rotations are linear, it's easy to extend the result to vectors of any length. Now, if v is (1,0), the result of the rotation will be
       ( cos(theta),  sin(theta) ).
How does this help us if v is an arbitrary unit vector? Given a unit vector v, let v' be the vector perpendicular to v, obtained by rotating v by pi/2. Now v and v' form an orthonormal basis, and relative to this basis, v has coordinates (1,0). But we've already found out what we get by rotating v by theta radians: relative to our new basis, the result must be
       ( cos(theta), sin(theta) ).
Relative to our original basis, this vector is
       cos(theta) v  +  sin(theta) v'
This is the result we're looking for: ``If you rotate a vector v by theta radians, you end up with cos(theta) v plus sin(theta) v,'' where v' is v, rotated by pi/2. Scaling v does not affect this result. A consequence of this result is that the mapping R that rotates vectors by theta radians is represented by the matrix
       +-                        -+
       |  cos(theta)  -sin(theta) |
       |                          |.
       |  sin(theta)   cos(theta) |
       +-                        -+
It is useful to note that R has this exact representation relative to any orthonormal basis where the second vector is obtained from the first by a rotation of pi/2. Top ## A canonical representation for rotations Suppose we have a rotation R, defined in three-dimensional space, that rotates vectors by angle theta about unit vector n. For an arbitrary vector r, we can break r up into two orthogonal components: one parallel to n and one perpendicular to n. We can call these components rParallel and rPerp. The two-dimensional diagram below shows this decomposition. All of the vectors lie in the plane containing r and n.
                    \           . rParallel
                     \          .
                      \         .
                    r  \        .
                        \       .
                         \      .
                          \     .
                           \    ^
                            \   |
                             \  |  n
                              \ |
                     ..........\|
                    rPerp
Now, what does R do to vectors that are perpendicular to n? Since R rotates each vector about n, if a vector v is perpendicular to n, then R(v) is perpendicular to n as well (remember that rotations preserve inner products, and orthogonality in particular). So rPerp just gets rotated in the plane perpendicular to n. We know from the last section how to find R(rPerp): if we let rPerp' be the vector obtained by rotating rPerp by pi/2 about n, then
       R(rPerp) = cos(theta) rPerp  +  sin(theta) rPerp'
We will also want to know what R(rPerp') is. Since rotating rPerp' by pi/2 about n yields -rPerp, applying our familiar formula to rPerp' gives us
       R(rPerp') = cos(theta) rPerp'  -  sin(theta) rPerp.
Now, since n, rPerp, and rPerp' are mutually orthogonal, these vectors form a basis. Since we can scale r so that rPerp has norm 1, and since rPerp' has the same norm as rPerp, we may assume that the basis is actually orthonormal. The matrix of R relative to this basis is
       +-                              -+
       |  1         0            0      |
       |                                |
       |  0     cos(theta)  -sin(theta) |.
       |                                |
       |  0     sin(theta)   cos(theta) |
       +-                              -+
Since the rotation we're representing is arbitrary, we've shown that every rotation can be represented by a matrix of the above form. Equivalently, every rotation matrix is similar to one of the above form. This fact justifies the use of the term ``canonical form.'' The canonical form we've found shows why three-dimensional rotations are very much like two-dimensional rotations: The effect of a three-dimensional rotation on any vector is to rotate the component of that vector that is normal to the rotation axis, and leave the component parallel to the rotation axis fixed. This rotation matrix is a useful ``model'' to keep in mind when dealing with rotations because of its particularly simple form. It's easy to read off some types of information directly from this matrix. Some examples: `--` The trace of the above matrix is 1 + 2 cos(theta). Since the trace of a matrix is invariant under similarity transformations, every rotation matrix has trace equal to 1 + 2 cos(theta). So we can easily find the rotation angle of any rotation matrix. `--` Every rotation has 1 as one of its eigenvalues. We already knew that, but there it is, sitting alone in its one-dimensional diagonal block. The other eigenvalues are complex unless the rotation angle is a multiple of pi. `--` Every rotation is an orthogonal mapping, that is, orthogonal vectors map to orthogonal vectors. This has to be true because the canonical form is an orthogonal matrix, represented relative to an orthonormal basis. Top ## Rotation axis and angle Our soccer ball model shows that a rotation has a fixed vector, called the ``axis.'' Now if the vector n is fixed by R, then -n is fixed as well, so the direction of the rotation axis is not unique. Given a rotation R and a vector v, normal to the rotation axis n of R, the angle between v and R(v), measured counterclockwise around n, is the rotation angle of R. We see that the rotation angle depends on the direction of the axis: if we pick -n as the axis, we change the sign of the angle. Note that while the rotation axis and angle of a rotation are not uniquely defined, a choice of axis and angle do determine a unique rotation. How do we find the rotation matrix R that rotates vectors by angle theta about the unit vector n? If n is
       n = (n1, n2, n3),
then
                                          2
       R  =   I   +   ( 1 - cos(theta) ) N   +   sin(theta) N,
where
           +-             -+
           |  0   -n3   n2 |
           |               |
       N = |  n3   0   -n1 |.
           |               |
           | -n2   n1   0  |
           +-             -+
How do we recover the rotation angle and axis of a rotation R from a corresponding rotation matrix, M? We've already seen in the ``canonical form'' section that the rotation angle is
       ACOS (  ( Trace(M) - 1 ) / 2  ).
If the rotation angle is not zero or pi, then the relation
            T
       M - M  = 2 sin(theta) N
allows us to recover the rotation axis n from M, while if the rotation angle is pi, we have
                  2
       M = I + 2 N,
again determining n. In the ``Mathematical road map'' chapter, we'll verify these assertions. Top ## Time-dependent coordinate transformations Suppose we have two bases, B1 and B2, where the elements of B2, expressed relative to B1, are time dependent:
       B2 = { v1(t), v2(t), v3(t) }.
An example of a time-dependent coordinate transformation is the transformation from J2000 to body equator and prime meridian coordinates. If R(t) transforms vectors from basis B1 to basis B2, the basis vectors of B2 are the rows of the matrix R(t). Let p(t) and p'(t) be position and velocity vectors expressed relative to B1. What is the corresponding velocity, expressed relative to B2? We know that p(t) has coordinates
       R(t) p(t)
relative to B2, so the time derivative of R(p(t)) is
       R(t) p'(t)  +  R'(t) p(t),
relative to B2. If R(t) is expressed as a product of the form
       R(t) = [ w1(t) ]   [ w2(t) ]   [ w3(t) ] ,
                       i           j           k
then
       R'(t)  =     [ w1(t) ]'  [ w2(t) ]   [ w3(t) ]
                             i           j           k

                 +  [ w1(t) ]   [ w2(t) ]'  [ w3(t) ]
                             i           j           k

                 +  [ w1(t) ]   [ w2(t) ]   [ w3(t) ]'
                             i           j           k
Since we know the explicit form of the factors (given in the ``Notation'' section), we can compute R'(t). We must take care when converting velocity vectors between systems whose bases are related in a time-dependent way. If R(t) varies extremely slowly, it is tempting to ignore the R' term, and in fact this is a valid approximation in some cases. However, since the magnitude of this term is proportional to the magnitude of p, the term can be large when R is quite slowly varying. An example: Let B1 be the basis vectors of the J2000 system, and let
       B2  =  { v1(t), v2(t), v3(t) }
be defined as follows: v1(t) is the geometric Jupiter-Sun vector at ephemeris time t, v3(t) is orthogonal to v1(t) and lies in the plane containing v1(t) and Jupiter's pole at time t, and v2(t) is the cross product of v3(t) and v1(t). Let R(t) be the transformation matrix from basis B1 to B2. Then the period of R(t) is 1 Jovian year (we're ignoring movement of Jupiter's pole). Now if p(t) is the Jupiter-Sun vector in J2000 coordinates, then p'(t) is the negative of Jupiter's velocity in J2000 coordinates. But in B2 coordinates, R(t) ( p(t) ) always lies along the x-axis, and if we approximate Jupiter's motion as a circle, then R(p(t))' is the zero vector. So we have the equation
       R(t) p'(t)  +  R'(t) p(t)  =  [ R(t)( p(t) ) ]'  =  0,
which implies
       R'(t)p(t)   =   - R(t) p'(t).
So in this case, the term involving R' has the same magnitude as the term involving R, even though R is slowly varying. Top ## Euler angles Given a rotation matrix M (usually representing a coordinate transformation), we occasionally have the need to express it as the product
       M  =  [w1]    [w2]    [w3]  .
                 i1      i2      i3
The angles w1, w2, and w3 are called ``Euler angles.'' It is not necessarily obvious that this ``factorization'' is possible. It turns out that as long as i2 does not equal i1 or i3, it is possible, for any rotation matrix M. In the ``Mathematical road map'' chapter, we exhibit the formulas for calculating w1, w2, and w3, given M and i1, i2, and i3. Top ## Quaternions Quaternions are four dimensional vectors, on which a particular kind of arithmetic is defined. The quaternions that have norm equal to 1 are called ``unit quaternions.'' Unit quaternions may be associated with rotations in the following way: if a rotation R has unit vector n = (n1, n2, n3) as an axis and w as a rotation angle, then we represent R by
       Q = ( cos(w/2),  sin(w/2) n1,  sin(w/2) n2,  sin(w/2) n3 ).
As you might suspect, this association is not unique: substituting (w + 2*pi) for w, we see that -Q is also a representation for R. If we choose the rotation axis and angle of R so that the angle lies in [0, pi], then there is a unique quaternion representing R, except in the case where R is a rotation by pi radians. Top ## Quaternion arithmetic CSPICE does not currently contain any routines that make use of quaternion arithmetic. Eventually, CSPICE may use quaternion multiplication to compose rotations, since quaternion arithmetic is more efficient than matrix multiplication. At present, this section is merely for the curious. Top ### Definitions There are two binary operations defined on quaternions: addition and multiplication. The main interest of quaternion multiplication is that we can actually carry out composition of rotations using the multiplication defined on the quaternions. If quaternions Q1 and Q2 represent rotations R1 and R2, then Q2*Q1 represents R2(R1). So the mapping from unit quaternions to rotations is a group homomorphism, where the ``multiplication'' operation on the rotations is functional composition. Quaternion addition is simple vector addition. Multiplication is a little more complicated. Before defining it, we're going to introduce a new notation for quaternions that makes it easier to deal with products. The quaternion
       Q = ( Q0, Q1, Q2, Q3 )
can be represented as
       Q0 + ( Q1, Q2, Q3 ),
or
       s + v,
where s represents the ``scalar'' Q0 and v represents the ``vector''
       ( Q1, Q2, Q3 ).
We define the ``conjugate'' of the quaternion
       q = s + v
as
        *
       q  = s - v.
Given two quaternions,
       q1 = s1 + v1,  q2 = s2 + v2,
we define the product q1 * q2 as
       ( s1 * s2 - < v1, v2 > )  +  ( s1 * v2  +  s2 * v1  +  v1 x v2 ).
We've grouped the ``scalar'' and ``vector'' portions of the product. Top ### Basic properties of multiplication Let's check out a few of the properties of the multiplication formula. Is multiplication commutative? No; if s1 and s2 above are zero, then the product is
       - < v1, v2 >   +   v1 x v2,
which is not commutative. However, multiplication is associative: given three quaternions q1, q2, and q3, we have
       q3 * ( q2 * q1 ) = ( q3 * q2 ) * q1.
We'll forgo checking this; it's messy but straightforward. If you do check it, the vector identities
        A x ( B x C ) =  < A, C > B  -  < A, B > C

       ( A x B ) x C  =  < C, A > B  -  < C, B > A
will be useful. What's the product of q and its conjugate? It comes out to
              2
       || q ||.
What's the conjugate of the product
       q1 * q2,
where q1 and q2 are as defined above? The product formula allows us to verify that the answer is
         *     *
       q2  * q1.
Top ### Deducing the multiplication formula One really interesting fact about the product formula is that it is a sum of binary operations, each of which is linear (where the coefficients are scalars, not quaternions) in both operands. This implies that the product formula itself is linear in q1 and q2. You can check this: if we scale q1 by x, the product gets scaled by x. The same thing happens if we scale q2. If we replace q1 by the sum of two quaternions, say
       q1 = q + q' =  ( s + s' )  +  ( v + v' ),
the product is
       q * q2   +   q' * q2.
The analogous result occurs when we replace q2 by a sum of two quaternions. Because of this linearity property, we can define multiplication on a small set of quaternions, and then define multiplication on the whole set of quaternions by insisting that the multiplication operator is linear in both operands. This gives us an equivalent definition of multiplication. To carry out this definition, we first define multiplication on the four quaternions
       1 + ( 0, 0, 0 ), which we call ``1,''
       0 + ( 1, 0, 0 ), which we call ``i,''
       0 + ( 0, 1, 0 ), which we call ``j,''
       0 + ( 0, 0, 1 ), which we call ``k.''
We treat ``1'' as a scalar and i, j, and k as vectors, and define the products
       1 * v   = v,  for v = i, j, k;

       v * v   = -1,  for v = i, j, k;

       v1 * v2 = - v2 * v1, for v1, v2 = i, j, k;

       i * j   = k;
       j * k   = i;
       k * i   = j.
Multiplication of i, j, and k works just like taking cross products. If we now proclaim that multiplication is linear in both operands, then since all quaternions can be expressed as linear combinations of ``1,'' i, j, and k, we've defined multiplication on the entire set of quaternions. You can check that this definition of multiplication is consistent with our formula above. Top ### Composing rotations using quaternions There is one last assertion to check: we've said that you can carry out composition of rotations using quaternion multiplication. Let's examine what that means: We've defined a mapping from quaternions to rotations, since the relation
       Q = ( cos(w/2),  sin(w/2) n1,  sin(w/2) n2,  sin(w/2) n3 )
allows us to recover w and the axis ( n1, n2, n3 ), hence the corresponding rotation. Now suppose we have two quaternions Q1 and Q2 that represent rotations R1 and R2, respectively. We're claiming that the product Q2 * Q1 represents R2(R1). So, we should be able to recover the rotation axis and angle of R2(R1) from the quaternion Q2 * Q1. In the ``Mathematical road map' chapter, we will verify this claim. Top # Mathematical road map The purpose of this chapter is to familiarize you with the mathematical ideas essential to dealing with rotations. If you understand the relevant mathematics, you are in a position to judge the merits of alternative software designs based on CSPICE routines. If you don't understand the mathematics, you can still build programs that work by paying careful attention to function interface specifications, but the design process is more error-prone, and you're unlikely to hit upon efficient and elegant solutions. The difference between the two perspectives is a bit like the difference between having a set of directions to get from point A to point B, and having a road map of the entire area. This chapter is not organized sequentially, since there is little logical dependence of one section on another. It is simply a collection of discussions. Top ## Rotation of a vector about an axis Suppose we have a unit vector n, and we wish to rotate a vector r about n by an angle of theta radians. What's the resulting vector? As in the tutorial discussion of the canonical form for rotations, we can express r as the sum of two orthogonal components:
       r  =  rParallel + rPerp.
Let's give the name rPerp' to the vector obtained by rotating rPerp by pi/2 radians about n. We know, from the results of the ``canonical form'' section, that applying our rotation to r will yield
       rParallel  +  cos(theta) rPerp  +  sin(theta) rPerp'
So all we have to do is find rPerp and rPerp' in terms of r, n, and theta. It turns out that rPerp' is precisely n x r, since n x r is parallel to rPerp' and has the same magnitude as rPerp, namely
       |r| sin(phi),
where phi is the angle between r and n. Rotating rPerp' by another pi/2 radians yields -rPerp, so
       rPerp = -n x ( n x r ).
In the picture below, `--` The diagonal, dashed line segment represents r. `--` The short, vertical, dashed line segment represents n. `--` The dotted, vertical extension of n represents the projection of r onto n. `--` The dotted, horizontal segments represent
       n x ( n x r)
`` on the right, and
       - n x ( n x r)
`` on the left. `--` The dotted, diagonal segment represents n x r. `--` The little boxes at the intersection of the segments are supposed to indicate orthogonality. `--` The ugly, little segments with the label ``phi'' between them are supposed to indicate the angle phi.
                          \           .  rParallel
                           \    phi --.
                            \ /       .
                          r  \        .
                              \       .
                               \      .
                                \     .
                                 \    ^
                                  \   |
                                   \  |    n
                                    \ |_
         - n x ( n x r )   ...........|_|.........   n  x  ( n x r )
                                     /_/
             = rPerp                .                     =  - rPerp
                                   .
                                  .
                                 .  n x r

                                         = rPerp'
Now we're ready to compute the image of r under the rotation. It is:
             rParallel     +   cos(theta) rPerp
                           +   sin(theta) rPerp'

       =   ( r - rPerp )   +   cos(theta) rPerp
                           +   sin(theta) rPerp'

       =        r          +   ( cos(theta) - 1 )   rPerp
                           +     sin(theta)         rPerp'

       =        r          +   ( 1 - cos(theta) )  ( n x ( n x r ) )
                           +      sin(theta)       (     n x r     ).
This is what we were after: an expression for the image of r under the rotation, given in terms of r, theta, and n. Top ## Formation of a rotation matrix from axis and angle In this section, we derive an expression for a rotation matrix that explicitly relates the matrix to the rotation axis and angle. This expression is valuable for understanding how to find the rotation axis and angle of a rotation matrix, as well as how to build a rotation matrix having a given rotation axis and angle. The problem of finding a quaternion corresponding to a specified rotation matrix is also solved by the expression derived here. What's the rotation matrix R that rotates vectors by theta radians about the vector n? If n is a unit vector, then the result of the last section implies that
       R * r  =  r     +   ( 1 - cos(theta) )  ( n x ( n x r ) )
                       +      sin(theta)       (     n x r     ),
for any vector r. Now, let
       n = (n1, n2, n3),
and define the matrix N by
           +-             -+
           |  0   -n3   n2 |
           |               |
       N = |  n3   0   -n1 |;
           |               |
           | -n2   n1   0  |
           +-             -+
this definition implies that
       N * r = n x r
for all r. So we can rewrite the above expression as
       R * r  =  r     +   ( 1 - cos(theta) )  ( N * ( N * r ) )
                       +      sin(theta)       (     N * r     ),
or
                                              2
       R * r  =  [  I  +  ( 1 - cos(theta) ) N  +  sin(theta) N  ]  r.
Since r is arbitrary, we must have
                                          2
       R  =   I   +   ( 1 - cos(theta) ) N   +   sin(theta) N.
R is the desired matrix. Top ## Finding the axis and angle of a rotation matrix The topic is covered in reference [1], so we'll just make a few notes. There are many ways to recover the rotation axis. The most elegant method we know of is presented in [1]. The idea is based on the observation that any rotation matrix R can be expressed by
                                          2
       R  =   I   +   ( 1 - cos(theta) ) N   +   sin(theta) N,
where N is derived from the rotation axis, as in the last section. Now N is skew-symmetric and N squared is symmetric, so
            T
       R - R   =  2 sin(theta) N.
As long as sin(theta) is non-zero, we've found N and hence the axis itself. If theta is pi, we have
                       2
       R  =   I  +  2 N,
which still allows us to recover the axis. In the tutorial section, we showed that the rotation angle can be recovered from the trace of a rotation matrix:
       angle = ACOS (  ( trace - 1 ) / 2  ).
If the angle is very small, we will determine it more accurately from the relation
            T
       R - R   =  2 sin(theta) N.
Top ## Formation of a rotation matrix from a quaternion Since the quaternion gives us a rotation's axis and angle, an earlier discussion in this chapter gives us one way of recovering the rotation matrix: twice the arccosine of the first component of the quaternion gives us the rotation angle, and the rest of the quaternion is the rotation axis, so AXISAR can be used to form the matrix. In this approach, we may want to treat small rotation angles as a special case, since the arccosine function is very inaccurate when the argument is close to 1. We would use the norm of the ``vector'' portion of the quaternion to give us the sine of half the rotation angle instead, and recover the rotation angle from this. There is a fast, accurate solution available. It depends on the formula relating a rotation matrix to its axis and angle, which we derived earlier in the chapter. In this approach, we compute the matrix corresponding to a quaternion, component by component. Define
       c = cos(theta/2),

       s = sin(theta/2),
and let the quaternion
       q  =   c   +  s n
          =   q0  +  s ( q1, q2, q3 )
represent a rotation R having unit axis vector n and rotation angle theta. If n = ( n1, n2, n3 ), and we define the matrix N by
           +-             -+
           |  0   -n3   n2 |
           |               |
       N = |  n3   0   -n1 |,
           |               |
           | -n2   n1   0  |
           +-             -+
then the matrix M representing R is
                                          2
       M  =   I   +   ( 1 - cos(theta) ) N   +   sin(theta) N.
Now we can make the substitutions
       sin(theta) = 2 c s,

                               2
       ( 1 - cos(theta) ) = 2 s
to obtain
                               2
       M  =   I   +   2 ( s N )   +   2 c ( s N ).
Substituting the elements of our quaternion into s N, we find
                                +-                                     -+
                                |     2    2                            |
               +-       -+      | -(q2 + q3 )     q1 q2        q1 q3    |
               | 1  0  0 |      |                                       |
               |         |      |                  2    2               |
       M  =    | 0  1  0 | + 2  |    q1 q2     -(q1 + q3 )     q2 q3    |
               |         |      |                                       |
               | 0  0  1 |      |                               2    2  |
               +-       -+      |    q1 q3        q2 q3     -(q1 + q2 ) |
                                +-                                     -+

                                +-                                     -+
                                |                                       |
                                |      0         -q0 q3       q0 q2     |
                                |                                       |
                                |                                       |
                           + 2  |     q0 q3         0        -q0 q1     |,
                                |                                       |
                                |                                       |
                                |    -q0 q2       q0 q1         0       |
                                +-                                     -+
so
           +-                                                          -+
           |           2    2                                           |
           | 1 - 2 ( q2 + q3 )    2 (q1 q2 - q0 q3)   2 (q1 q3 + q0 q2) |
           |                                                            |
           |                                                            |
           |                               2    2                       |
       M = | 2 (q1 q2 + q0 q3)    1 - 2 ( q1 + q3 )   2 (q2 q3 - q0 q1) |.
           |                                                            |
           |                                                            |
           |                                                    2    2  |
           | 2 (q1 q3 - q0 q2)    2 (q2 q3 + q0 q1)   1 - 2 ( q1 + q2 ) |
           |                                                            |
           +-                                                          -+
Top ## Equivalence of rotation definitions The idea discussed here is used implicitly throughout the CSPICE rotation routines. We wish to prove that definitions (1) and (2) from the ``Definition of rotations'' section of the tutorial are equivalent. To do this, we need to show that a mapping R that satisfies definition (1) also satisfies definition (2). This amounts to showing that R has a fixed subspace of dimension 1, or equivalently, that R has 1 as one of its eigenvalues. Top ### An algebraic approach We observe that the characteristic polynomial of a rotation is of degree three, and so has either zero or two complex roots, hence at least one real root. Because rotations preserve norms, the magnitudes of all of the roots (eigenvalues), real or complex, are equal to one. So the real roots are 1 or -1. The determinant of any rotation matrix is 1, since the determinant of any 3 by 3 matrix is the dot product of the third column with the cross product of the first and second columns, and for rotations, this cross product is the third column. But the determinant is also the product of the eigenvalues. In the case where all three roots are 1 or -1, we cannot get a product of 1 unless at least one eigenvalue is equal to 1. If there are complex roots, they are complex conjugates, so their product is 1, which implies that the real root must be 1 as well, if the product of all three roots is 1. Top ### A geometric approach Again, we assume that our rotation R satisfies definition (1), and we prove that R has a fixed axis. We're going to look at the effect of R on the unit sphere, and demonstrate that two points on the sphere are fixed. We'll assume that the rotation is not the identity and does not map any vector v to -v. This last case corresponds to a rotation of pi radians. Our first observation is that R maps great circles to great circles. This follows from the fact that a great circle is a set of unit vectors, all orthogonal to some particular vector v. Since R preserves inner products, the image of the great circle is a set of unit vectors, all orthogonal to R(v). Now, consider the distances that vectors on the unit sphere move when the rotation R is applied; there is some vector v, not necessarily unique, that moves the maximum distance. Let C1 be a great circle passing through v and R(v), and let C2 be a great circle that passes through v and intersects C1 at right angles. Now R(C2) passes through R(v), and if we can show that it passes through at right angles to C1, then C2 and R(C2) intersect at vectors p and -p, both of which are normal to v and R(v). So R(p) is either p or -p. But we've assumed that R does not map any vector to its inverse, so R(p) = p, and we have a fixed vector. So, we must show that R(C2) passes through R(v) at right angles to C1. If it did not, there would be some point w on C2, close to v, such that
       || R(w) - w ||  >  || R(v) - v ||,
contradicting our hypothesis that no vector moves farther that v. We will leave the rigorous proof of this last assertion to the energetic reader. Top ## Quaternion multiplication In this section, we verify some claims made in the tutorial on rotations. There are two assertions that we need to prove: `1.` If the unit quaternion q represents the rotation R, then for any vector v,
                         *
       R(v)  =  q * v * q,
`` where v is treated as a quaternion. `2.` If the unit quaternions q1 and q2 represent the rotations R1 and R2, then the rotation R2(R1) is represented by the quaternion
       q2 * q1.
Top ### Assertion 1 To prove the first assertion, we express R(v) in the form
       R(v) =  v + sin(theta) n x v  + ( 1 - cos(theta) ) n x ( n x v ),
where n is a unit axis vector and theta is the corresponding rotation angle. We also define the constants C and S by
       C = cos(theta/2),
       S = sin(theta/2).
The quaternion
       q = C  +  S n
represents R. To check the assertion, we compute
            ( C  +  S n ) * v * ( C  -  S n )

       =    ( C  +  S n ) * [ ( S  <v,n> )  +  ( C v  -  S v x n ) ]

                                               2
       =    [ C S <v, n>  -  S C < n, v >  +  S  < n,  v x n > ]

               2                    2
         +  [ C v  - C S v x n  +  S <v, n> n  +  S C n x v

             2
         -  S n x ( v x n ) ].
Since n is normal to v x n, the scalar part of the last line is zero, which leaves us with
        2       2                              2
       C v  +  S <v, n> n  +  2 S C n x v  -  S n x ( v x n ).
We can re-write this again as
        2       2                               2
       C v  +  S <v, n> n  +  2 S C n x v  + 2 S n x ( n x v )

                                                2
                                           -   S n x ( n x v ),
and using the vector identity
       A x ( B x C ) =  < A, C > B  -  < A, B > C,
we can modify the final term to arrive at
        2       2                               2
       C v  +  S <v, n> n  +  2 S C n x v  + 2 S n x ( n x v )

                                                2
                                           -   S ( <n, v> n - <n, n> v ).
Since n is a unit vector, the entire expression reduces to
                                     2
            v  +  2 S C n x v  +  2 S  n x ( n x v )

       =    v  +  2 sin(theta/2) cos(theta/2) n x v

                       2
               +  2 sin (theta/2) n x ( n x v)

       =    v  +  sin(theta) n x v  +  ( 1 - cos(theta) ) n x ( n x v )

       =    R(v).
Top ### Assertion 2 The second assertion follows rather more quickly from the first. Given that R1(v) is
                  *
       q1 * v * q1 ,
we can express R2(R1(v)) by
                            *      *
          q2 * ( q1 * v * q1 ) * q2
                                       *
       =  ( q2 * q1 ) * v * ( q2 * q1 ).
Now let q be a quaternion that represents R2(R1); then
                *
       q * v * q   =  R2(R1(v))
for all v. We'll be done if we can show that, in general, for unit quaternions x and y, if
                *             *
       x * v * x  =  y * v * y
for all vectors v, then x equals y or -y. But this equation implies that
        *                 *
       y * x * v  =  v * y * x,
for all v, which in turn implies that
        *
       y * x
is a scalar, since only scalar quaternions commute with every vector quaternion (due to the cross product term in the product formula). Since y and x are unit quaternions, either
        *
       y * x = 1
or
        *
       y * x = -1,
so x = y or -y. We conclude that q2 * q1 = q or -q, so q2 * q1 does represent R2(R1). Top ## Recovery of Euler angles from a rotation matrix Here's the problem: Given a rotation matrix M, and a set of coordinate axes indexed by i1, i2, i3, find angles w1, w2, w3 such that
       M = [w1]     [w2]      [w3]  .                       (1)
               i1       i2        i3
There are a couple of reasons why we might want to solve this problem: first, the representation of a rotation by three Euler angles is a common one, so it is convenient to be able to convert the matrix representation to this form. Also, the three angles on the right hand side of equation (1) often allow you to visualize a rotation more readily than does the matrix representation M. This ``factorization'' is possible if i2 does not equal i1 or i3. For each valid sequence (i1-i2-i3) of axes, there is a set of functions that give us w1, w2, and w3 as a function of M:
       w1 = f1         ( M ),
              i1-i2-i3

       w2 = f2         ( M ),
              i1-i2-i3

       w3 = f3         ( M ).
              i1-i2-i3
How can we derive the functions
       f1        ,  f2        ,  f3        ?
         i1-i2-i3     i1-i2-i3     i1-i2-i3
One approach is to multiply the matrices on the right hand side of equation (1); this yields a matrix whose entries are sums of products of sines and cosines of w1, w2, and w3. We can then equate the entries of this matrix to those of M, and find formulas for w1, w2, and w3 that arise from the component-wise correspondence. In subsequent sections, we actually carry out this procedure for 3-1-3 and 1-2-3 factorizations. There are twelve sets of axes to consider, so there are potentially twelve sets of functions to compute. However, the procedure we've just described is not enjoyable enough to justify doing it twelve times. We'd like to find a slicker way of solving the problem. One approach is to find a way of ``recycling'' the formulas we derived for one particular axis sequence. Here's an example of how we might do this: Suppose that we already have functions
       f1     ,  f2     ,  f3
         3-1-3     3-1-3     3-1-3
that allow us to factor rotation matrix M as a 3-1-3 product: If
       M = [w1]   [w2]    [w3] .                            (2)
               3      1       3
then
       w1 = f1      ( M ),
              3-1-3

       w2 = f2      ( M ),
              3-1-3

       w3 = f3      ( M ).
              3-1-3
We'd like to somehow use the functions we've already got to factor M as a 2-3-2 product: we want to find functions
       f1     ,   f2     ,   f3
         2-3-2      2-3-2      2-3-2
such that
       M = [y1]   [y2]   [y3] ,                             (3)
               2      3      2
and
       y1 = f1      ( M ),
              2-3-2

       y2 = f2      ( M ),
              2-3-2

       y3 = f3      ( M )
              2-3-2
without having to derive
       f1     ,   f2     ,   f3
         2-3-2      2-3-2      2-3-2
from scratch. We'll start out by using a new basis, relative to which the right hand side of (3) is not a 2-3-2, but rather a 3-1-3 rotation. It is important to note here that bases are ordered sets of vectors; changing the order changes the basis. Let the basis B1 be the ordered set of vectors
       {e(1), e(2), e(3)},
and let the basis B2 be the ordered set of vectors
       {e(3), e(1), e(2)}.
Now the rotation matrix
       [y]
          2
expressed relative to B1 represents the same rotation as the matrix
       [y]
          3
expressed relative to B2. Both matrices represent a rotation of y radians about the vector e(2). Similarly, the matrix
       M  =  [y1]  [y2]  [y3]
                 2     3     2
expressed relative to B1 represents the same rotation as the matrix
       M' =  [y1]  [y2]  [y3]
                 3     1     3
expressed relative to B2. So if C is the matrix whose columns are the elements of B2, expressed relative to B1, namely
            +-       -+
            | 0  1  0 |
       C =  | 0  0  1 |,
            | 1  0  0 |
            +-       -+
then
        -1
       C   M  C   =  M'                                     (4)
We can use the functions
       f1     ,  f2     ,  f3
         3-1-3     3-1-3     3-1-3
to factor M' as a 3-1-3 product: applying (4), we have
                  -1
       y1 = f1 ( C   M  C ),                                (5)

                  -1
       y2 = f2 ( C   M  C ),                                (6)

                  -1
       y3 = f3 ( C   M  C ),                                (7)
so we've found functions that yield the angles y1, y2 and y3 that we sought. ``No muss, no fuss.'' How much mileage can we get out of our 3-1-3 factorization functions? Looking at our example, we see that the main ``trick'' is to find a basis so that the factorization we want is a 3-1-3 factorization with respect to that basis. It is important the new basis be right-handed; otherwise the form of the matrices
       [w]
          i
is not preserved. It turns out that for any axis sequence of the form a-b-a, we can find a right-handed basis such that the factorization we want is a 3-1-3 factorization with respect to that basis. There are two cases: if we define a successor function s on the integers 1, 2, 3 such that
       s(1) = 2,
       s(2) = 3,
       s(3) = 1,
we either have b = s(a) or a = s(b). In the first case, b = s(a), and if our original ordered basis is
       B1 = { e(1), e(2), e(3) },
then
       B2 = { e(b), e( s(b) ), e(a) }
is the right-handed basis we're looking for. You can check that
       e(a) = e(b) x e( s(b) ).
We recall that the transformation matrix C we require has the elements of B2 as columns. For example, if a is 2 and b is 3, then B2 is
       { e(3), e(1), e(2) },
and the matrix C is
            +-       -+
            | 0  1  0 |
       C =  | 0  0  1 |,
            | 1  0  0 |
            +-       -+
as we have seen previously. The axis sequences that can be handled by the above procedure are 1-2-1, 2-3-2, and 3-1-3. In the second case, a = s(b), and if our original ordered basis is
       B1 = { e(1), e(2), e(3) },
then
       B2 = { e(b), -e( s(a) ), e(a) }
is the right-handed basis we're looking for. Again, you can verify this by taking cross products. The transformation matrix C we require has the elements of B2 as columns. For example, if a = 2 and b = 1, then B2 is
       { e(1), -e(3), e(2)) }
and the matrix C is
            +-       -+
            | 1  0  0 |
       C =  | 0  0  1 |.
            | 0 -1  0 |
            +-       -+
The axis sequences that can be handled by the above procedure are 1-3-1, 2-1-2, and 3-2-3. So we can use our 3-1-3 formula to handle all of the a-b-a factorizations, just by computing the correct transformation matrix C. What about a-b-c factorizations? As you might guess, the procedure we've described also applies to these, with very little modification. Suppose we have the formulas we need to carry out a 1-2-3 factorization. We'd like to find a basis that allows us to represent the a-b-c product
       [w1]   [w2]   [w3]
           a      b      c
as the product
       [w1]   [w2]   [w3] .
           1      2      3
Again, there are two cases, depending on whether b is the successor of a or a is the successor of b, according to our cyclic ordering. In the case where b is the successor of a, the right-handed basis we want is
       B2 = { e(a), e(b), e(c) }.
With respect to the basis B2, our a-b-c factorization is a 1-2-3 factorization. Again, we can form the transformation matrix C by letting its columns be the elements of B2. In the second case, a is the successor of b. Our new basis is
       B2 = { e(a), e(b), -e(c)}.
In this case, there is a slight twist: the change of basis we use negates the third rotation angle. This is not a serious problem; the change of basis converts the product
       [w1]   [w2]   [w3]
           a      b      c
to
       [w1]   [w2]   [-w3] ,
           1      2       3
so we can still recover the angles w1, w2, and w3 easily. So our 1-2-3 factorization formula allows us to handle all the a-b-c factorizations. Having shown that we can perform all of the a-b-a and a-b-c factorizations using just one formula for each type of factorization, we now proceed to derive those formulas. This is not a particularly instructive procedure, but the derivations ought to be written down somewhere, and this is as good a place as any. Top ### Euler angle recovery: a-b-a case We'll derive the formulas for a 3-1-3 factorization. In this case, the right hand side of (1) is
       +-                     -+     +-                      -+
       |  cos(w1)  sin(w1)  0  |     | 1       0        0     |
       | -sin(w1)  cos(w1)  0  |  *  | 0    cos(w2)  sin(w2)  |  *
       |      0       0     1  |     | 0   -sin(w2)  cos(w2)  |
       +-                     -+     +-                      -+

       +-                     -+
       |  cos(w3)  sin(w3)  0  |
       | -sin(w3)  cos(w3)  0  |
       |     0        0     1  |
       +-                     -+
which equals
       +-                     -+
       |  cos(w1)  sin(w1)  0  |
       | -sin(w1)  cos(w1)  0  |   *
       |      0       0     1  |
       +-                     -+
       +-                                            -+
       |          cos(w3)       sin(w3)         0     |
       |  -cos(w2)sin(w3)   cos(w2)cos(w3)   sin(w2)  |
       |   sin(w2)sin(w3)  -sin(w2)cos(w3)   cos(w2)  |
       +-                                            -+
which comes out to
       +-                                                              -+
       |         cos(w1)cos(w3)          cos(w1)sin(w3)  sin(w1)sin(w2) |
       | -sin(w1)cos(w2)sin(w3)  +sin(w1)cos(w2)cos(w3)                 |
       |                                                                |
       |        -sin(w1)cos(w3)         -sin(w1)sin(w3)  cos(w1)sin(w2) |.
       | -cos(w1)cos(w2)sin(w3)  +cos(w1)cos(w2)cos(w3)                 |
       |                                                                |
       |         sin(w2)sin(w3)         -sin(w2)cos(w3)         cos(w2) |
       +-                                                              -+
At this point, we can recover w1, w2, and w3 from the elements of M. The inverse trigonometric functions used below are borrowed from Fortran. We find w2 from the relation
       w2 = ACOS( M(3,3) ).
(So w2 is in [0, pi].) If w2 is not equal to 0 or pi, then we can recover w1 as follows:
       M(1,3)       sin(w1)sin(w2)
       ------   =   --------------  =  tan(w1),
       M(2,3)       cos(w1)sin(w2)

       w1 = ATAN2 ( M(1,3), M(2,3) ).
We find w3 in an analogous fashion, again assuming w2 is not equal to 0 or pi. We find
        M(3,1)       sin(w2)sin(w3)
       -------   =   --------------  =  tan(w3),
       -M(3,2)       sin(w2)cos(w3)

       w3 = ATAN2 ( M(3,1), -M(3,2) ).
Note the minus sign used in the second ATAN2 argument. For ATAN2 to determine the correct value, it is necessary that the first and second arguments have the same signs as sin(w3) and cos(w3), respectively. Now if w2 is equal to zero or pi, we have a degenerate case: M is the product of two rotations about the third coordinate axis. The angles of the rotations are not determined uniquely, only the sum of the angles is. One way of finding a factorization is to set w3 to zero, and solve for w1. The matrix M then is equal to
       +-                                 -+
       |  cos(w1)  cos(w2)sin(w1)     0    |
       | -sin(w1)  cos(w2)cos(w1)     0    |,
       |    0            0         cos(w2) |
       +-                                 -+
so we can recover w1 by computing
       w1 = ATAN2( -M(2,1), M(1,1) ).
Top ### Euler angle recovery: a-b-c case We'll derive the formulas for a 1-2-3 factorization. In this case, the right hand side of (1) is
       +-                      -+     +-                      -+
       | 1       0        0     |     | cos(w2)   0  -sin(w2)  |
       | 0    cos(w1)  sin(w1)  |  *  |    0      1      0     |  *
       | 0   -sin(w1)  cos(w1)  |     | sin(w2)   0   cos(w2)  |
       +-                      -+     +-                      -+

       +-                      -+
       |  cos(w3)  sin(w3)  0   |
       | -sin(w3)  cos(w3)  0   |
       |     0        0     1   |
       +-                      -+
which equals
       +-                      -+
       | 1       0        0     |
       | 0    cos(w1)  sin(w1)  |  *
       | 0   -sin(w1)  cos(w1)  |
       +-                      -+

       +-                                              -+
       | cos(w2)cos(w3)   cos(w2)sin(w3)      -sin(w2)  |
       |                                                |
       |       -sin(w3)          cos(w3)          0     |
       |                                                |
       | sin(w2)cos(w3)   sin(w2)sin(w3)       cos(w2)  |
       +-                                              -+
which comes out to
       +-                                                              -+
       |         cos(w2)cos(w3)          cos(w2)sin(w3)        -sin(w2) |
       |                                                                |
       |        -cos(w1)sin(w3)          cos(w1)cos(w3)  sin(w1)cos(w2) |
       | +sin(w1)sin(w2)cos(w3)  +sin(w1)sin(w2)sin(w3)                 |.
       |                                                                |
       |         sin(w1)sin(w3)         -sin(w1)cos(w3)  cos(w1)cos(w2) |
       | +cos(w1)sin(w2)cos(w3)  +cos(w1)sin(w2)sin(w3)                 |
       +-                                                              -+
We recover w2 by
       w2 = ASIN ( -M(1,3) ),
so w2 is in the interval [-pi/2, pi/2]. As long as w2 does not equal pi/2 or -pi/2, we can find w1 by the formula
       w1 = ATAN2 ( M(2,3), M(3,3) ),
and w3 from the formula
       w3 = ATAN2 ( M(1,2), M(1,1) ).
If w2 is -pi/2 or pi/2, we have a degenerate case. The sum of w1 and w3 is determined, but w1 and w3 are not determined individually. We can set w3 to zero, which reduces our right hand side to
       +-                                       -+
       |         0            0        -sin(w2)  |
       |  sin(w1)sin(w2)    cos(w1)       0      |,
       |  cos(w1)sin(w2)   -sin(w1)       0      |
       +-                                       -+
so we can recover w1 from the formula
       w1 = ATAN2 ( -M(3,2), M(2,2) ).
Top # Appendix A: Document Revision History Top ### May 27, 2010 Minor edit to eliminate typo. Top ### November 17, 2005 Documentation of the routines qxq_c, qdq2av_c was added. Top ### January 10, 2005 A few corrections were made to environment tags in the .ftm source for this document. Top ### February 2, 2004 Performed a spell-check on text. Top ### December 2, 2002 `` The relationship between Euler angles and the C-matrix is defined differently by different projects. Modifications have been made to clarify the definitions used by Cassini, Voyager and Galileo. Top ### April 26, 1999 `` An equation involving quaternion multiplication was corrected: the expression v*v = 0 was replaced by v*v = -1. `` Quotation style was changed from British to American. `` Some variable names were changed to remove underscores. `` Some minor re-wording was done to simplify creation of the CSPICE version of this document.