Path: Orbit/OrbitMechanics
% Launch azimuth to achieve a desired orbit inclination. -------------------------------------------------------------------------- Form: az = AZLaunch( i, lat ) -------------------------------------------------------------------------- ------ Inputs ------ i (1,:) Desired inclination (deg) lat Latitude (deg) ------- Outputs ------- az Launch azimuth (deg) -------------------------------------------------------------------------- References: Wiesel, W. E., Spaceflight Dynamics, McGraw-Hill, 1988, pp. 76-77. --------------------------------------------------------------------------
Common: Graphics/Plot2D
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