力传感器静态自动推力校准算法  

Static Autothrust Calibration Algorithm of Force Sensor

作　　者：郭健鑫 郑科 凌思睿[1] 王得志[1] 马帅 Guo Jianxin;Zheng Ke;Ling Sirui;Wang Dezhi;Ma Shuai(Beijing Institute of Aerospace Testing Technology,Beijing 100074)

机构地区：[1]北京航天试验技术研究所,北京市100074

出　　处：《仪器仪表标准化与计量》2023年第3期22-24,共3页Instrument Standardization & Metrology

摘　　要：本文针对姿轨控发动机点火试车试验的推力测量,为提高试验前的推力校准效率,保障试验进度,基于推力校准的操作规程,设计开发了一种力传感器静态自动推力校准算法。算法经硬件平台验证,结果证明其适用可行。Aiming at the thrust measurement of attitude and orbit control engine ignition test,in order to improve the efficiency of thrust calibration before the test and ensure the test progress,the paper designs and develops a static automatic thrust calibration algorithm of force sensor based on the operating procedures of thrust calibration.The algorithm is verified by hardware platform,and the results show that it is feasible.

关 键 词：姿轨控发动机 推力测量 静态推力校准 自动化推力校准 

分 类 号：V463[航空宇航科学与技术—航空宇航制造工程]