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。

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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。

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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

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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。

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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。

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