Path: Orbit/Glideslope
Calculate delta-Vs for a pulsed circumnavigation.
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Form:
[dVM, t, x] = GlideslopeCircumnav( x0, w, N, T, rho, a )
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Inputs
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x0 (6,1) Relative state in LVLH frame (m, m/s)
w (1) Orbit rate (rad/sec)
N (1) Number of pulses, default is 4.
T (1) Period of circumnavigation (s), default is 1 orbit period
rho (1) Radius of circumnavigation (m), leave empty to calculate from x0
a (3,1) Orbit normal of circumnavigation ([0;1;0] produces in-plane)
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Outputs
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dVM (3,N) Delta-V in LVLH frame
t (1,N) Times to apply the delta-V
x (3,N) State at each delta-V point (before maneuver)
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Reference: Hablani, Tapper, Bashian et al. "Guidance algorithms
for Autonomous Rendezvous of Spacecraft with a Target
Vehicle in Circular Orbit," 2001
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Orbit: Glideslope/CWSimAndPlot Orbit: Glideslope/ClohessyWiltshire Orbit: Glideslope/DVGlideslope SC: BasicOrbit/OrbRate Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Math: Linear/Mag Math: Linear/Unit Math: Solvers/NewtRaph
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