约束条件下水平冲量多弧段交会机动方案设计

The Horizontal Impulse Multi-Segmental Arcs Rendezvous Project Designed in Restricted Condition

在交会过程的近距离寻的段 ,由于地面观测条件和追踪航天器燃料的限制 ,提出了固定时间交会和最大燃料消耗量的约束问题。本文探讨在此条件下 ,如何实现水平冲量多弧段交会机动。分析了交会过程中每一次机动的决定性因素 ,给出了解算满足两个过程约束条件的迭代算法 ,仿真算例表明了该算法的可行性。

On the short-rang homing phase of rendezvous, we bring forward a question which is about given rendezvous time and maxium fuel wastage in restricted condition of land observation and tracking spacecraft′s fuel. This paper studies how to realize the Horizontal Impulse Multi-Segmental Arcs Rendezvous in this case.We analysis determining factor of every maneuvering flight and present an iterative algorithms which can satisfy the restricted condition. Result of simulation shows the algorithms is feasible.