Path: FormationFlying/Utility
% Computes the time in seconds until the latitude "theta2" is reached from the original latitude, "theta1". Since version 7. -------------------------------------------------------------------------- ------ Inputs ------ a (1) Semimajor axis [km] w (1) Argument of perigee [rad] e (1) Eccentricity theta0 (1) Initial argument of latitude [rad] theta1 (1) Final argument of latitude [rad] mu (1) Gravitational constant [km^3/sec^2] (optional) ------- Outputs ------- dT (1) Time until next theta is reached [sec] --------------------------------------------------------------------------
AC: ACData/ACTConstants SC: BasicOrbit/E2M SC: BasicOrbit/Nu2E SC: BasicOrbit/Nu2M SC: SCData/sCTConstants Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Database/Constant Common: General/CellToMat Common: General/DeleteCell Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Math: Linear/DupVect Math: Trigonometry/WrapPhase
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