LowThrustRendezvousSim:

% Simulation of low thrust maneuver to rendezvous with target orbit.
 Applies constant magnitude, variable direction thrust to optimally
 change each element one at a time, according to specified order.
--------------------------------------------------------------------------
   Form:
   [t,el,r,v,mass,acc,accRSW] = LowThrustRendezvousSim( ...
     el0, elT, mass0, thrust, Isp, elemOrder, mu);
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   el0         (1,6)     Initial orbital elements
   elT         (1,6)     Target orbital elements
   mass0       (1,1)     Initial mass
   thrust      (1,1)     Thrust
   Isp         (1,1)     Specific impulse
   elemOrder   (1,5)     Order in which to change elements
   mu          (1,1)     Gravitational constant

   -------
   Outputs
   -------
   t           (1,:)     Simulation time vector
   el          (:,6)     Orbital elements
   r           (3,:)     Inertial position
   v           (3,:)     Inertial velocity
   mass        (1,:)     Mass
   acc         (3,:)     Accleration in inertial frame
   accRSW      (3,:)     Acceleration in RSW (radial / tangent / normal)

--------------------------------------------------------------------------
   See also: LowThrustTimeToTransfer, LowThrustGVE_EventFcn, LowThrustGVERHS
--------------------------------------------------------------------------

Children:

Common: Database/Constant
Common: Graphics/NewFig
Common: Graphics/ODETimeDisplay
Common: Graphics/Plot2D
Common: Graphics/TimeLabl
Math: Linear/Cross
Math: Linear/Unit
Missions: AsteroidProspector/GVEGuidance
Missions: AsteroidProspector/LowThrustGVERHS
Missions: AsteroidProspector/LowThrustGVE_EventFcn
Missions: AsteroidProspector/LowThrustTimeToTransfer
Orbit: OrbitCoord/OrbElemDiff
OrbitMiniToolbox: Support/El2RV
SC: BasicOrbit/Period