无拖曳卫星推力器动态模型研究

doi:10.3969/j.issn.1674-1579.2016.01.010

Abstract

Abstract: Abstract：DragFree technology is a key technology for future space exploration, which put forward higher requirements for thrusters. The development and application of micro thrusters for dragfree satellites are introduced based on the investigation of dragfree technology space application. According to the development requirement for Chinese dragfree propulsion, the dynamic model of the mass flow control of proportional valve for dragfree cold gas micro thruster is built. A fuzzy adaptive PID controller is then proposed to improve the dynamic characteristics.

Key words: Keywords：dragfree satellite, micro thruster, proportional valve, fuzzy PID controller

CLC Number:

HU Qi-Yang, CHEN Jun, LONG Jun, FAN Xu-Feng. The Dynamic Model of Thruster for DragFree Satellite[J]., 2016, 42(1): 52-56.

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URL: http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/10.3969/j.issn.1674-1579.2016.01.010

http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/Y2016/V42/I1/52

References

［1］LANGE B. The control and use of dragfree satellite［D］. Stanford: Stanford University,1964. ［2］DEBRA D B. Propulsion requirement for dragfree satellite［J］. Journal of Spacecraft and Rockets, 1971,8(4):412-414. ［3］罗子人,白姗,边星,等. 空间激光干涉引力波探测［J］. 力学进展, 2013, 43(4):434-441. LUO Z R, BAI S, BIAN X, et al. Space laser interferometry gravitational wave detection ［J］ Advances in Mechanics,2013, 43(4): 434-441. ［4］STEIGER C, ROMANAZZO M, EMANUELLI P P, et al. Flying at the edgeextremely low altitude operations for ESA’s dragfree gravity mission GOCE［C］//AIAA Guidance, Navigation, and Control Conference. Washington D.C.:AIAA,2013：19-22. ［5］ZIEMER J K, MERKOWITZ S M. Microthrust propulsion for the LISA mission［C］//The 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.Washington D.C.:AIAA,2004. ［6］汪旭东,范旭丰,陈君，等. 微小冷气比例推力器模块的数据驱动PID控制策略［J］. 信息与控制,2014,43(3):381-384. WANG X D, FAN X F, CHEN J, et al. Datadriven PID control of cold gas microProportion thruster module［J］.Information and Control,2014,43(3):381-384. ［7］黄勇. 新型电液比例阀的设计及其控制方法的研究［D］.长沙:湖南大学,2007. ［8］吴根茂,邱敏秀,王庆丰,等.新编实用电液比例技术［M］.杭州:浙江大学出版社,2006:23-24. ［9］方锦辉,孔晓武,魏建华. 伺服比例阀的非线性建模与实验验证［J］. 浙江大学学报, 2014,48(5):784-790. FANG J H, KONG X W, WEI J H. Nonlinear modeling and validation of a servosolenoid valve［J］. Journal of Zhejiang University,2014,48(5):784-790. ［10］张国良,曾静, 柯熙政,等. 模糊控制及其MATLAB应用［M］.西安:西安交通大学出版社,2002:85-96.

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The Dynamic Model of Thruster for DragFree Satellite

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