GlideslopePlanner:

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)
--------------------------------------------------------------------------
   Form:
   [dV, t, xM] = GlideslopePlanner( x0, w, d )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   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

   -------
   Outputs
   -------
   dV      (3,:)    Delta-Vs (m/s)
   t       (1,:)    Time (sec)
   xM      (3,:)    State at each delta-V point (before maneuver)

--------------------------------------------------------------------------
   See also CWSimAndPlot, Glideslope, GlideslopeCircumnav.
--------------------------------------------------------------------------

Children:

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
Orbit: Glideslope/CWSimAndPlot
Orbit: Glideslope/ClohessyWiltshire
Orbit: Glideslope/DVGlideslope
Orbit: Glideslope/GlideslopeCircumnav
SC: BasicOrbit/OrbRate

Back to the Orbit Module page