InPlane:
--------------------------------------------------------------------------
Computes the delta-v's required for an in-plane maneuver.
Since version 7.
--------------------------------------------------------------------------
------
Inputs
------
meas_elem (1,6) Reference orbital elements (Alfriend format)
[a,theta,i,q1,q2,W]
delta_elem (:,6) Error in orbital element differences (Alfriend format)
accNom (1) Nominal acceleration [km/s/s]
dTMin (1) Minimum achievable burn duration [sec]
nOrbMin (1) Minimum number of orbits maneuver may last
nOrbMax (1) Maximum number of orbits maneuver may last
horizon (1) Minimum amount of time required prior to first burn [sec]
-------
Outputs
-------
burnData (.) Array of burn data structures with burn times,
durations, magnitudes and directions.
t0 (1) First burn time [sec from meas time]
tF (1) Final burn time [sec from meas time]
nBurns (1) Number of burns required
--------------------------------------------------------------------------
Children:
Common: Database/Constant
FormationFlying: Control/OptimalInPlaneDeltaV
FormationFlying: Utility/TimeUntilTheta
Math: Trigonometry/WrapPhase
