Path: FormationFlying/Coord
% Calculates orbital elements for an in-line formation. -------------------------------------------------------------------------- Form: elSet = ProjLine( aRef, iRef, kSats, rF ) -------------------------------------------------------------------------- ------ Inputs ------ aRef (1,1) Semi-major axis of reference orbit [km] iRef (1,1) Inclination of reference orbit [rad] kSats (1,1) Number of satellites rF (1,1) Distance between satellites [km] ------- Outputs ------- elSet (kSats,6) Orbital elements of all spacecraft rH (3,kSats) Radius vector in Hills frame [km] vH (3,kSats) Velocity vector in Hills frame [km/s] --------------------------------------------------------------------------