rendezvous method

In this paper, a method of solving quadratic equations-based four-impulse optimal rendezvous between near circular orbits is investigated.

在引入平均轨道概念的基础上，提出了一种针对低轨道卫星的过顶与成像区域时间的快速预报算法。

After that, an elliptic orbit two-impulse guidance method is introduced. Furthermore, this paper also gives a kind of nonlinear guidance method for space rendezvous.

最后，在椭圆参考轨道相对运动模型的基础上，研究了椭圆参考轨道的二脉冲交会制导策略。此外，本文还给出了一种空间交会的非线性制导方法。

According to the target spacecraft ′ s orbit height and the chaser spacecraft ′ s orbit height, the design method of the target ′ s initial phase for the rendezvous orbit was presented.

根据目标飞行器轨道高度和追踪飞行器入轨轨道高度，给出了目标飞行器交会对接轨道初始相位的设计方法。

The method of intelligent control applied to the orbital control of rendezvous and docking phase of spacecraft is presented in this paper.

本文介绍了将智能控制方法用于航天器交会对接段的轨道控制。

A Method of Intelligent Control for Rendezvous and Docking of Space Station and Its Simulation

空间站交会对接的一种智能控制方法与仿真