Path: OpticalNavigation/Dynamics
% Right-hand-side for a 2 dimensional planet takeoff. -------------------------------------------------------------------------- Form: d = RHSPlanet2D xDot = RHSPlanet2D( x, ~, a, beta ) -------------------------------------------------------------------------- ------- Inputs ------- x (4,1) State vector [x;y;vX;vY] t (1,1) Time (s) (unused) a (1,1) Thruster acceleration beta (1,1) Thrust angle from the horizontal (rad) ------- Outputs ------- xDot (:,1) d[x;y;vX;vY]/dt --------------------------------------------------------------------------
Math: Linear/Mag
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