AutoFormGeometry:
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Define new geometric goals for a single satellite, such that any semi-major
axis difference is eliminated, and the new trajectory maintains a minimum
separation distance from all other team members trajectories in the team.
Command ONLY along-track offset, set radial oscillation to 0, and leave
out-of-plane motion unchanged.
For each OTHER member, compute the extreme y-values, and determine the closest y0
whose extrema are at least minSepDist from all OTHER extrema
Since version 7.
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Usage:
newGoals = AutoFormGeometry( state, memberGoals, minSepDist, maxSepDist, nS, maxIter );
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Inputs
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state (.) Orbital state data structure
memberGoals (.) Geometric goals for all other members in the cluster
minSepDist (1) Minimum allowable separation distance between satellites
minSepDist (1) Maximum allowable separation distance between satellites
nS (1) Number of samples to use in computing 1-period trajectories
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Outputs
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newGoals (.) Goals data structure defining desired relative motion for team
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Children:
FormationFlying: Coord/IsCircGeom
FormationFlying: Dynamics/HillsEqns
FormationFlying: EccDynamics/FFEccGoals
FormationFlying: EccDynamics/FFEccLawdensEqns
FormationFlying: EccDynamics/FFEccYExt
FormationFlying: Guidance/NearestOffset
FormationFlying: Transformation/DeltaElem2Goals
FormationFlying: Transformation/FFEccDeltaElem2Goals
FormationFlying: Transformation/FFEccDeltaElem2Hills
FormationFlying: Transformation/FFEccGoals2Hills
FormationFlying: Transformation/FFEccHills2DeltaElem
FormationFlying: Transformation/Goals2Hills
Math: Trigonometry/UnwrapPhase
Orbit: OrbitCoord/El2Alfriend
OrbitMiniToolbox: Support/M2Nu
SC: BasicOrbit/OrbRate
SC: BasicOrbit/Period
