| 飞行器最佳冗余测量 |
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| 引用本文： | 薛沛丰. 飞行器最佳冗余测量[J]. 宇航学报, 1988, 0(3) |
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| 作者姓名： | 薛沛丰 |
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| 作者单位： | 上海工业大学 |
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| 摘 要： | 本文在提出测量精度、故障检测性和故障识別性指标的基础上,研究了冗余测量元件的安装型式和最佳安装方位;提出了一种故障冗余处理方法,以提高故障识别的可靠性,并指出了正交-斜装组合型结构,在飞行器冗余测量中,是一种较好的安装结构。
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| 关 键 词： | 储备技术 仪表定向 余度飞行控制系统 冗余校验 |
OPTIMAL REDUNDANT MEASUREMENTS OFVEHICLE |
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| Xue Peifeng. OPTIMAL REDUNDANT MEASUREMENTS OFVEHICLE[J]. Journal of Astronautics, 1988, 0(3) |
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| Authors: | Xue Peifeng |
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| Affiliation: | Shanghai University of Technology |
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| Abstract: | On the basis of presenting performance index of measurement accuracy, failure detectability and identifiability, optimal mounting configurations and orientations of redundant measurers are investigated in this paper. Failure redundant management is propounded for raising reliability of failure identification. It is pointed out that orthogonal-skew mounting configuration is a better method to measure flight parameters. |
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| Keywords: | Redundancy technique Instrument orientation Redundant flight control system Redundant ckeck |
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