Generalized multiple-revolution Lambert algorithm for solving multiple-impulse rendezvous problem 广义多圈Lambert算法求解多脉冲最优交会问题
The dynamics model of rendezvous and docking, optimal rendezvous problem and the framework of the rendezvous and docking simulation system are studied in this thesis. 本文对交会对接仿真所需的动力学模型、空间交会的最优控制和交会对接仿真系统的总体框架进行了深入研究,并建立了交会对接仿真的原型系统。
A two-maneuver guidance law is designed for the two-impulse rendezvous problem. 本文针对两冲量交会问题,设计出两次机动的制导方案。
Solution for optimal 3-impulse rendezvous problem 三脉冲最优交会问题的解法
In this paper, the minimum-fuel, multiple-impulse, time-fixed rendezvous problem based on the linearized relative motion equation is investigated. 本文研究了两个空间飞行器在固定时间内燃料最省的多冲量交会问题。
Solving the Optimal Multi-impulse Rendezvous Problem Based on the Dynamic Programming 利用动态规划原理实现多冲量最优交会问题
Rendezvous and docking technology is a key technology for the second step of China manned spaceflight project. The mission plan for phasing maneuvers is a critical problem of rendezvous trajectory design and control. 交会对接技术是我国载人航天工程二期需要掌握的关键技术,远程导引变轨任务规划是交会对接轨道设计与控制的关键问题之一。