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] --------------------------------------------------------------------------