| 运载火箭制导系统惯性器件误差补偿方法研究 |
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| 引用本文： | 王广民.运载火箭制导系统惯性器件误差补偿方法研究[J].航天控制,1997(4). |
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| 作者姓名： | 王广民 |
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| 作者单位： | 北京航天自动控制研究所!100854 |
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| 摘 要： | 提供了对运载火箭制导系统惯性器件的各项主要误差在飞行中进行实时补偿的方法，以提高运载火箭将卫星送入轨道的精度。文中以中等精度惯性器件为例，对运载火箭计算其补偿效果。
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| 关 键 词： | 运载火箭 制导系统 补偿 |
Research on Compensation Methods of Inertial Unit Errors of Launch Vehicle Guidance System |
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| Wang Guangmin.Research on Compensation Methods of Inertial Unit Errors of Launch Vehicle Guidance System[J].Aerospace Control,1997(4). |
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| Authors: | Wang Guangmin |
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| Institution: | Beijing Aerospace Antomatic Control Institute 100854 |
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| Abstract: | The real - time compensation methods to correct main errors of intertial units ofguidance system in launch vehicle during fligut is introduced. Orbit injecion accuracies ofsatellites is improved by using these methods. In this paper, taking inertial units of mediumaccuracy as example, compensation the to errors of launch vehicles is calculated. |
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| Keywords: | Launch vehicle Guidance system Compensation |
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