火箭发动机喷管伺服机构负载模拟系统设计与实验

doi:10.3969/j.issn.1000-1093.2014.09.024

摘要/Abstract

摘要： 针对火箭发动机喷管伺服机构的半物理仿真需要，设计一种可对惯性负载、摩擦力矩负载、弹性力矩负载、伺服机构安装刚度进行模拟的电液负载模拟系统。依据伺服机构负载特点，由机械的方式实现惯性负载、摩擦负载以及安装刚度的模拟，由阀控伺服马达实现弹性力矩的模拟；分别建立伺服机构系统和马达加载系统的数学模型，并为马达加载系统设计基于速度前馈补偿和力矩前馈的控制系统；进行负载模拟器的现场实验，实验结果表明，各种加载负载满足精度要求，验证了负载模拟器设计的合理性和实用性，以及控制策略的有效性。

关键词: 兵器科学与技术, 负载模拟, 伺服机构, 数学模型, 力矩前馈, 速度补偿

Abstract: A new electro-hydraulic torque load simulator is proposed for the semi-physical simulation of the servo mechanism in launch vehicle, which could simulate the inertia load, friction and elastic torques, and servo mechanism mounting rigidity. On the basis of load characteristics of servo mechanism, the inertia , friction, and servo mechanism mounting rigidity are simulated for the mechanical structures, and the elastic load is simulated for the servomotor. The complete mathematical models of the motor loading system and the servo mechanism system are constructed. A control system of the servo mechanism is designed based on speed compensation and torque feed-forward. Some field tests of load simulation device were made. The test results show that the various loads meet accuracy requirements. The proposed design is reasonable and practicable, and the control system is effective.

Key words: ordnance science and technology, load simulation, servo mechanism, mathematical model, torque feed-forward, speed compensation

中图分类号:

TG262

张朋，付永领，郭彦青. 火箭发动机喷管伺服机构负载模拟系统设计与实验[J]. 兵工学报, 2014, 35(9): 1495-1502.

ZHANG Peng, FU Yong-ling, GUO Yan-qing. Design and Experiment of Load Simulation System for Servo Mechanism of Rocket Engine Nozzle[J]. Acta Armamentarii, 2014, 35(9): 1495-1502.

参考文献

［1］延皓，李长春，陈策. 伺服机构综合负载模拟试验系统［J］.兵工学报, 2012, 33(5):588-593.
YAN Hao, LI Chang-chun, CHEN Ce. Comprehensive load simulation system of servo mechanism［J］. Acta Armamentarii, 2012, 33(5):588-593. (in Chinese)
［2］张洁，孙凝生. 运载火箭伺服机构负载模拟与空载特性间的转换传递函数［J］. 航天测控，2002,18(2):12-16.
ZHANG Jie, SUN Ning-sheng. The transfer function between servo sector load of launch vehicle load and no-load characteristics［J］. Aerospace Control, 2002, 18(2): 12-16. (in Chinese)
［3］郝经佳，赵克定，许宏光. 刚度、惯量负载对电液负载仿真台性能影响的研究［J］. 中国机械工程，2002,13(6)：458-460.
HAO Jing-jia, ZHAO Ke-ding, XU Hong-guang. Study on the influence of rigidity and inertia in electro-hydraulic load simulator［J］. China Mechanical Engineering, 2002, 13(6):458-460. (in Chinese)
［4］张朋，付永领，郭彦青. 伺服机构负载模拟系统设计与实验研究［J］. 液压与气动，2013（12）：34-37.
ZHANG Peng, FU Yong-ling, GUO Yan-qing. Design and experimental investigation of load simulation of servo mechanism［J］. Chinese Hydraulics & Pneumatics, 2013(12):34-37. (in Chinese)
［5］华清. 电液负载模拟器关键技术的研究［D］. 北京：北京航空航天大学，2001.

HUA Qing. Study on the key technology of electro-hydraulic load simulator［D］. Beijing: Beihang University, 2001. (in Chinese)
［6］朱晓敏, 延皓, 孙萌. 多自由度伺服机构负载模拟系统建模与实验研究［J］. 兵工学报，2011, 32(5):602-606.
ZHU Xiao-min, YAN Hao, SUN Meng. Modeling and experimental investigation of load simulator of multiple DOF servo mechanism［J］. Acta Armamentarii, 2011, 32(5):602-606. (in Chinese)
［7］孙萌, 李长春, 延皓, 等. 多自由度伺服机构负载模拟系统动态特性研究［J］. 兵工学报, 2013, 34(3):378-384.
SUN Meng, LI Chang-chun, YAN Hao, et al. Study on dynamic performance of multiple-DOF servo mechanism's load simulator system［J］. Acta Armamentarii, 2013, 34(3):378-384. (in Chinese)
［8］ Shang Yaoxing, Jao Zongxia, Wang Xiaodong, et al. Study on friction torque loading with an electro-hydraulic load simulator［J］. Chinese Journal of Aeronautics, 2009,22(6): 691-699.
［9］姚建勇, 焦宗夏. 改进型LuGre模型的负载模拟器摩擦补偿［J］，北京航空航天大学学报，2010, 36(7):812-815.
YAO Jian-yong, JIAO Zong-xia. Friction compensation for hydraulic load simulator based on improved LuGre friction model［J］. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(7):812-815. (in Chinese)
［10］刘丽兰, 刘宏昭, 吴子英, 等. 机械系统中模型的研究进展［J］，力学进展，2008, 38(2):201-213.
LIU Li-lan, LIU Hong-zhao, WU Zi-ying, et al. An overview of friction models in mechanical［J］. Advances in Mechanics, 2008, 38(2):201-213. (in Chinese)
［11］刘金琨. 先进PID控制MATLAB仿真［M］. 北京:电子工业出版社，2013:56-58.
LIU Jin-kun. MATLAB simulation of advanced PID control ［M］. Beijing:Publishing House of Electronics Industry, 2013:56-58. (in Chinese)
［12］刘长年. 液压伺服系统的分析与设计［M］. 北京:科学出版社，1985.
LIU Chang-nian. Analysis and design of the hydraulic servo system［M］. Beijing: Science Press,1985. (in Chinese)

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