Path: Orbit/Glideslope
% Calculate sequential glideslope maneuvers for planning purposes.
These algorithms apply only to circular orbits. Contains default data for an
inbound slope, circumnavigation, and outbound slope (array of 3 segments)
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Form:
[dV, t, xM] = GlideslopePlanner( x0, w, d )
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Inputs
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x0 (6,1) Initial relative state (m, m/s)
w (1) Orbit rate
d (:) Structure of data for glideslope segments
.N (1) Number of pulses
.T (1) Period for segment (sec)
.rTarget (3,1) or (1) Target vector or radius
.a (3,1) Orbit normal for circumnavigation
.V (2,1) Commanded velocity for glideslope
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Outputs
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dV (3,:) Delta-Vs (m/s)
t (1,:) Time (sec)
xM (3,:) State at each delta-V point (before maneuver)
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See also CWSimAndPlot, Glideslope, GlideslopeCircumnav.
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Orbit: Glideslope/CWSimAndPlot Orbit: Glideslope/ClohessyWiltshire Orbit: Glideslope/DVGlideslope Orbit: Glideslope/GlideslopeCircumnav 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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