Path: Orbit/OrbitManeuver
% Computes inclination drift for geosynchronous orbits. Use this function to plan north/south stationkeeping. -------------------------------------------------------------------------- Form: [dV, dT, dI] = DVIDrift( box, year, doPlot ) -------------------------------------------------------------------------- ------ Inputs ------ box (1,1) Size of stationkeeping box (deg) year (1,:) Year of maneuvers doPlot (1,1) Create a plot ------- Outputs ------- dV (1,1) Delta V per maneuver (m/sec) dT (1,:) Time between maneuvers (days) dI (1,:) Change in inclination -------------------------------------------------------------------------- Reference: Agrawal, B. N. (1986). Design of Geosynchronous Spacecraft. Prentice-Hall, Englewood Cliffs, NJ. --------------------------------------------------------------------------
Common: Graphics/Plot2D
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