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SUPPORT SITE |
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SUPPORT SITE |
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Path: SC/Visualization
% Plots one orbit and the sun vector looking down on the ECI Plane. The input is a set of Kepler elements and a Julian date. It also plots the line of nodes and the line between apogeee and perigee, and, optionally, a spin axis located at the beginning of the orbit. Specify a planet name to use SunVectorECI instead of SunV1. Has two built-in demos, one for an Earth orbit and one for Mars. Since version 1. -------------------------------------------------------------------------- Form: h = PltOrbit( el, jD, uSpin, planet ) -------------------------------------------------------------------------- ------ Inputs ------ el (1,6) Orbital elements [a i W w e M] jD (1,1) Julian date uSpin (3,1) Spin axis (optional) planet (1,:) Planet name (optional) ------- Outputs ------- h (1,1) Figure handle -------------------------------------------------------------------------- See also: SunV1, SunVectorECI, PlotPlanet, AxesCart, Axis3D --------------------------------------------------------------------------
Common: Database/Constant Common: General/Watermark Common: Graphics/AxesCart Common: Graphics/Axis3D Common: Graphics/NewFig Common: Time/Date2JD SC: BasicOrbit/CP2I SC: BasicOrbit/E2Nu SC: BasicOrbit/El2RV SC: BasicOrbit/M2EEl SC: Ephem/SunV1 SC: Ephem/SunVectorECI SC: Visualization/PlotPlanet
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