Research on Instantaneous Thrust Measurement for Attitude-control Solid Rocket Motor

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.

作 者： OUYANG Hua-bing WANG Jian-ping LIN Feng XU Wen-gan   作者單位： OUYANG Hua-bing(Scool of Mechanical Engineering,Tongji university,Shanghai,200092,China;Zhexi Branch College, Zhejiang University of Technology, Quzhou 324000, China)

WANG Jian-ping,LIN Feng(Zhexi Branch College, Zhejiang University of Technology, Quzhou 324000, China)

XU Wen-gan(College of Mechanical Engineering, Zhejiang University of Technology, Hangzhou 310014, China) 

刊 名： 兵工學(xué)報(bào)（英文版）  英文刊名： JOURNAL OF CHINA ORDNANCE  年，卷(期)： 2008 4(2)  分類(lèi)號(hào)： V435  關(guān)鍵詞： spacecraft structure and design   solid rocket motor   instantaneous thrust   dynamic compensation