|
SUPPORT SITE |
|
|
|
SUPPORT SITE |
|
Path: Orbit/OrbitMechanics
% Computes the longitudinal motion due to an acceleration a -------------------------------------------------------------------------- Form: [lon, lond] = LonMot( lon0, lond0, a, t ) -------------------------------------------------------------------------- ------ Inputs ------ lon0 Initial longitude lond0 Initial longitude rate a Acceleration t Time ------- Outputs ------- lon Longitude (rad) lond Longitude rate --------------------------------------------------------------------------
Common: Graphics/Plot2D
Back to the Orbit Module page