[1]冀 哲,姚晓先,梁作宝.变刚度电动负载力矩模拟系统的刚度解算[J].弹箭与制导学报,2017,37(5):30-34.[doi:10.15892/j.cnki.djzdxb.2017.05.001]
 JI Zhe,YAO Xiaoxian,LIANG Zuobao.The Stiffness Calculating of the Variable Stiffness Electric Loading Simulator[J].,2017,37(5):30-34.[doi:10.15892/j.cnki.djzdxb.2017.05.001]
点击复制

变刚度电动负载力矩模拟系统的刚度解算

参考文献/References:

[1] LEONDES C T, PEARSON J L. Missile autopilot adaption using control-surface hinge-moment feedback[J]. Journal of Spacecraft and Rockets, 1968, 5(2): 154-159.
[2] ANTONELLI M G, BUCCI G, CIANCETTA F, et al. Automatic test equipment for avionics Electro-Mechanical Actuators(EMAs)[J]. Measurement, 2014, 57: 71-84.
[3] YALLA S K, KAREEM A, KABAT S, et al. Dynamic load simulator: development of a prototype[J]. Journal of Engineering Mechanics, 2001, 127(12): 1310-1315.
[4] SHANG Yaoxing, YUAN Hang, JIAO Zongxia, et al. Matching design of hydraulic load simulator with aerocraft actuator[J]. Chinese Journal of Aeronautics, 2013, 26(2): 470-480.
[5] NAM Yoonsu. QFT force loop design for the aerodynamic load simulator[J]. IEEE Transactions on Aerospace and Electronic Systems, 2001, 37(4): 1384-1392.
[6] ULLAH N, KHATTAK M I, KHAN W. Fractional order fuzzy terminal sliding mode control of aerodynamics load simulator[C]//SAGE. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering.[S.l.:s.n.], 2015.
[7] WANG Xingjian, WANG Shaoping, WANG Xiaodong. Electrical load simulator based on velocity-loop compensation and improved fuzzy-PID[C]// IEEE. 2009 ISIE 2009 IEEE International Symposium on Industrial Electronics. [S.l.]:IEEE, 2009: 238-243.
[8] WANG X, WANG S, YAO B. Adaptive robust torque control of electric load simulator with strong position coupling disturbance[J]. International Journal of Control, Automation and Systems, 2013,11(2):325-332.
[9] ULLAH N, WANG S. Improved torque control of electrical load simulator with parameters and state estimation[J]. International Science Index, Electrical and Computer Engineerings, 2011, 5(2):1647-1653.
[10] 姚晓先, 宋晓东, 梁作宝, 等. 闭环负载刚度变化装置: CN102122135A[P]. 2011-07-13.
[11] 钱杏芳, 林瑞雄, 赵亚男. 导弹飞行力学 [M]. 北京: 北京理工大学出版社, 2011: 22-23.
[12] SACHS H K. Criteria of design for progressive torsion-bar springs[J]. Experimental Mechanics, 1967, 7(3): 105-109.
[13] LIN W F, CLARKE M D. Factors influencing the accuracy of aerodynamic hinge-moment prediction:ADA 066 606[R]. [S.l.:s.n.],1978.
[14] SCHROCDER M. Synthesis of low-peak-factor signals and binary sequences with low autocorrelation(Corresp.)[J]. IEEE Transactions on Information Theory, 1970, 16(1): 85-89.

备注/Memo

作者简介:冀哲(1987-),男,河北石家庄人,博士研究生,研究方向:机电伺服系统与检测技术

更新日期/Last Update:

2017-08-15