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A new approximate analytical method for the two-body impulsive orbit rendezvous problem with short range is presented. The classical analytical approach derives the initial relative velocity from the state transition matrix of linear relative motion equations. This paper proposes a different analytical approach based on the relative Lambert solutions. An approximate expression for the transfer time...
A new solution to the two-point boundary value problem for power-limited non-coplanar elliptic orbital rendezvous with constant thrust is proposed based on the linear relative motion equations. The process of rendezvous is composed of three time intervals, i.e., the first engine maneuver, a coasting subarc, and the second engine maneuver. An analytical propagation of the relative state is obtained...
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