Optimal trajectories are obtained by using a direct adjoining approach (so called the D form Lagrangian)for the interception or the rendezvous of a target in low circular Earth orbit by a vehicle which is initially in a high orbit.

 
  • 航天器從高軌道向位于低地球圓軌道的靶目標實(shí)施攔截或進(jìn)行交會(huì ) ,并用間接求解的直接伴隨方法 ,即用D型拉格朗日方法求解其優(yōu)化問(wèn)題。
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