| 平台防飞软件的设计依据 |
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| 引用本文： | 陈乃川.平台防飞软件的设计依据[J].航天控制,1994(3). |
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| 作者姓名： | 陈乃川 |
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| 作者单位： | 北京航天自动控制研究所 |
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| 摘 要： | 本文叙述了在导弹控制系统试验中因平台倒台而造成飞转的基本原理，为了控制国平台飞转而造成的故障损失，提出建立平台防飞软件的设计依据。
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| 关 键 词： | 导弹试验 平台 软件 |
The Basis for Designing a Software to prevent a platform from Runaway |
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| Chang Naichuan.The Basis for Designing a Software to prevent a platform from Runaway[J].Aerospace Control,1994(3). |
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| Authors: | Chang Naichuan |
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| Institution: | Beijing Aerospace Automatic Control Institute |
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| Abstract: | In the process of testing a missile control system, a platform runaway may be occurred owing to breakdown of supply source for the platform or other failures in the platform servo loop. A method using software to Prevent that situation being occurred thus minimize the loss is proposed in this paper. |
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| Keywords: | Missile test Plaghrm Software |
| 本文献已被 CNKI 等数据库收录！ |
