trim.inp: Trim template file
Fx   Fy   Fz   Mx   My   Mz                                                                   Aircraft forces and moments to trim
 1    1    1    1    1    1                                                                   
Fx   Fy   Fz   Mx   My   Mz                                                                   Optional trim values (default is 0)
0.0  0.0  0.0  0.0  0.0  0.0                                                                  
Fx    Fy    Fz    Mx    My    Mz                                                              Trim tolerance (fraction of weight)
.0002 .0002 .0002 .0002 .0002 .0002                                                           
Coll Lat Long Pedal Throttle Tilt Flap1 Flap2 Elev Rudder Addl                                Pilot controls
 1    1   1    1     0        0    0     0     0    0      0                                   
Roll Pitch Sideslip                                                                           Attitude controls used to trim
 1    1     0                                                                                 
Number of aerodynamic components (rotors and wings) used to trim                              
2                                                                                             
Comp RPM Coll Lat Long Tilt Flaps(4) Controls used by each aero component                     
 1    0   1    2   3    0    0    0   0   0                                                   Aero Component 1: Main rotor
 2    0   4    0   0    0    0    0   0   0                                                   Aero Component 2: Tail rotor
Ctrl Zero Coll  Lat  Long  Pedal  Throttle Tilt Flap1 Flap2 Elev Rudder Addl Mixer: Component/Pilot control gains
 1    0.0  1.0  0.0  0.0   0.0     0.0     0.0  0.0   0.0   0.0  0.0    0.0                   Rotor 1 Col 1:1 with Pilot Col Stick
 2    0.0  0.0  1.0  0.0   0.0     0.0     0.0  0.0   0.0   0.0  0.0    0.0                   Rotor 1 Lat 1:1 with Pilot Lat Stick
 3    0.0  0.0  0.0  1.0   0.0     0.0     0.0  0.0   0.0   0.0  0.0    0.0                   Rotor 1 Lon 1:1 with Pilot Lon Stick
 4    0.0  0.0  0.0  0.0   1.0     0.0     0.0  0.0   0.0   0.0  0.0    0.0                   Rotor 2 Col 1:1 with Pilot Pedal
Initial Pilot Control Settings Based on the Gains Above
          20.0  0.0  0.0   0.0     0.0     0.0  0.0   0.0   0.0  0.0    0.0
