| 航天飞行器交会对接段的姿态控制四元数法 |
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| 引用本文： | 程国采.航天飞行器交会对接段的姿态控制四元数法[J].航天控制,1991(2). |
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| 作者姓名： | 程国采 |
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| 作者单位： | 中国人民解放军国防科学技术大学 |
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| 摘 要： | 本文研究利用四元数作为误差信号进行航天飞行器姿态控制的控制规律,应用Pontrgagin极小原理导出了喷咀最优控制开关曲线,所得结果不仅可用于交会对接段也适用于航天飞行器上升段和返回段的姿态控制。
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| 关 键 词： | 航天器 航天器对接 航天器会合 姿态控制 四元数 |
THE METHOD FOR RENDEZVOUS AND DOCKING PHASE OF SPACE VEHICLE ATTITUDE CONTROL USING OUATERNION |
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| Cheng Guacai.THE METHOD FOR RENDEZVOUS AND DOCKING PHASE OF SPACE VEHICLE ATTITUDE CONTROL USING OUATERNION[J].Aerospace Control,1991(2). |
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| Authors: | Cheng Guacai |
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| Institution: | Cheng Guacai |
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| Abstract: | This paper presents a formula for control equations in which the control error is expressed as a quaternion and used to space vehicle attitude control system.The qpplication of the minimum principle of Pontryagin to control law of RCS is presented in this paper.The re- sults not only can be used to the rendezvous and docking phase but also canbe used to ascent phase and re-entry phase of space vehicle. |
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| Keywords: | Spacecraft Spacecraft docking Spacecraft randezvous Attitude control Quaternion |
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