AccelVector2ManeuverStruct:
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Build a "maneuver" data structure from acceleration and time vectors.
Since version 7.
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Usage:
[maneuver,dV,dT] = AccelVector2ManeuverStruct( aC, t, tRef, nomAccel, minSepTime );
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Inputs
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aC (3,N) [x;y;z] acceleration over N time intervals [km/sec^2]
t (1,N) Time vector [sec]
tRef (.) Reference time (epoch) [sec]
nomAccel (1) Magnitude of thruster's nominal acceleration output [km/sec^2]
minSepTime (1) Minimum allowable separation time between burns [sec]
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Outputs
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maneuver (.) Maneuver data structure
dV (1,k) Absolute value of all non-zero delta-v's [km/sec^2]
dT (1,N-1) Vector of time-steps [sec]
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Children:
FormationFlying: DataStructures/Maneuver_Structure
Math: Linear/Mag
Math: Linear/Unit
