https://sourceforge.net/p/odtbx/wiki/CalculateTrueAnomalyStep/Recent changes to CalculateTrueAnomalyStepenTue, 08 Jul 2014 17:34:12 -0000https://sourceforge.net/p/odtbx/wiki/CalculateTrueAnomalyStep/<div class="markdown_content"><p><strong>CALCULATE TRUE ANOMALY STEP</strong> Calculate the Orbit True Anomaly using the initial position and velocity. </p> <blockquote> <p>function f = calculateTrueAnomaly(initialStates) </p> </blockquote> <p>INPUTS: </p> <blockquote> <p><em>initialStates</em> - <span>[x0 y0 z0 x0dot y0dot z0dot]</span> Initial position and velocity in m and m/s. </p> </blockquote> <p>OUTPUTS: </p> <blockquote> <p><em>newStep</em> - New step dependant on true anomaly for orbit. </p> </blockquote> <p>Return to: <span>[MatlabJatAdaptor]</span></p></div>Tue, 08 Jul 2014 17:34:12 -0000https://sourceforge.net85ec17275b7b070619ed78b14d571926cc618dc0