SafeGuidanceSim:

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  Relative dynamic simulation for two LEO satellites with safe guidance.
  Includes differential disturbance forces for J2, drag and solar.
  Explicitly calls SafeGuidance maneuver planning algorithm.
 
  Assumptions:
   - satellites have different masses 
   - satellites have differential area for solar pressure
   - satellites have differential area for drag
   - disturbances do not measurably affect reference orbit over simulation

   Since version 10.
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  Form:
  simData = FFRelSim( simOptions )
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  Sim options fields:
    elRef  [a,i,W,w,e,M]
    nOrbits
    nPts     Discretization points per orbit
    distOpt  Flags for [solar drag J2]
    harmonicOrder
    control
    params
    noise
    flags
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Children:

AeroUtils: AtmosphericCalculations/AtmDens2
Common: Time/JD2000
FormationFlying: EccDynamics/FFEccLinOrb
FormationFlying: SafeGuidance/SafeEllipseParams
FormationFlying: SafeGuidance/SafeEllipsePosVel
FormationFlying: SafeGuidance/SafeGuidance
FormationFlying: Transformation/Hills2LVLH
FormationFlying: Transformation/LVLH2Hills
Math: Linear/Cross
Math: Linear/Mag
Math: Linear/Unit
Orbit: OrbitCoord/Alfriend2El
OrbitMiniToolbox: Support/M2E
SC: BasicOrbit/M2NuAbs
SC: BasicOrbit/OrbRate
SC: BasicOrbit/Period
SC: BasicOrbit/RVFromKepler
SC: Ephem/Eclipse
SC: Ephem/SunV2