orbital rendezvous

H_ ∞ Hypo-Optimal Control for Spacecraft Orbital Rendezvous

飞行器轨道交会的H∞次优控制问题

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An efficient adaptive filtering scheme is successfully used in the state and parameter estimation for the orbital rendezvous of earth synchronous satellites.

本文将一种有效的自适应滤波方案成功地应用于地球同步卫星轨道交会时的状态估计与参数估计之中。

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Research on Multiple-Impulse Fast Orbital Rendezvous Based on Lambert Theory

基于lambert理论的多脉冲快速轨道交会研究

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Coplanar orbital transfer with finite thrust based on the rendezvous concept is studied.

基于交会概念研究了卫星在平面内的最省燃料有限推力轨道转移问题.

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Small satellite orbital rendezvous is designed using the geometric logic of spherical triangle and the STK ( Satellite Tool Kit) software.

利用球面三角形的几何关系进行了基于STK（卫星工具包）的小卫星轨道交会的规划和设计。

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The problem on orbital rendezvous of spacecraft is a crucial technology for human space exploration. It is one of the most difficult problems in theory and application of spacecraft control.

空间在轨交会是载人航天技术中的关键问题之一，是目前航空控制理论与实践中的难点之一。

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Laser orbital rendezvous apparatus

轨道会合用激光装置

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Time-optimal fuel-fixed orbital rendezvous with multiple impulses

燃料受限的时间最优多脉冲交会问题

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State and parameter estimation for the orbital rendezvous of earth synchronous satellites

地球同步卫星轨道交会时的状态估计与参数估计

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General Strategies for Orbital Rendezvous

航天器轨道交会的一般策略

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Coplanar Orbital Transfer with Finite Thrust Based on Rendezvous Concept

基于交会概念的最省燃料共面有限推力轨道转移方法

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The main consideration is the orbital control precision of orbit maneuver. Finally, through the whole orbital dynamics simulation, based on the high target orbit rendezvous mission, the verification of the orbital maneuver strategy is feasible.

最后本文通过全轨道动力学仿真，验证了基于高轨目标交会飞行任务的轨道机动策略是可行的。

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Orbital maneuver is the primary condition for satellite autonomy, and it is the basis of phase keeping, phase maneuver and rendezvous.

卫星轨道机动是卫星自治的首要条件，它是相位保持、相位机动、交会对接的基础。

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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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