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Research on Instantaneous Thrust Measurement for Attitude-control Solid Rocket Motor
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作者 欧阳华兵 汪建平 +1 位作者 林峰 徐温干 《Defence Technology(防务技术)》 SCIE EI CAS 2008年第2期123-127,共5页
In order to measure the instantaneous thrust of a certain attitude-control solid rocket motor, based on the analysis of the measurement principles, the difference between the instantaneous thrust and steady thrust mea... In order to measure the instantaneous thrust of a certain attitude-control solid rocket motor, based on the analysis of the measurement principles, the difference between the instantaneous thrust and steady thrust measurements is pointed out. According to the measurement characteristics, a dynamic digital filter compensation method is presented. Combined the identification-modeling, dynamic compensation and simulation, the system's dynamic mathematic model is established. And then, a compensation digital filter is also designed. Thus, the dynamic response of the system is improved and the instantaneous thrust measurement can be implemented. The measurement results for the rocket motor show that the digital filter compensation is effective in the instantaneous thrust measurement. 展开更多
关键词 太空船结构 设计方法 固体燃料推进火箭发动机 瞬间冲击力
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