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GAO Feng, TANG Sheng-jing, SHI Jiao, GUO Jie. Compound control allocation strategy of dual aero/jet vane control missile[J]. JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY, 2012, 21(4): 434-441.
Citation: GAO Feng, TANG Sheng-jing, SHI Jiao, GUO Jie. Compound control allocation strategy of dual aero/jet vane control missile[J].JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY, 2012, 21(4): 434-441.

Compound control allocation strategy of dual aero/jet vane control missile

  • Received Date:2011-08-12
  • To solve the control allocation problem of dual aero/jet vane control missile, dynamics equations in longitudinal plane are derived, and the structure of compound control loop is designed based on attitude autopilot. Four brief compound control allocation strategies are researched and analyzed. Furthermore, a new strategy called chain combination variable proportional coefficient strategy based on rudder effect is presented. By simulation of initial climb trajectory, the characteristics of all the strategies are researched, and the results illustrate that the new strategy can meet the requirement well.
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  • [1]
    Gao Feng, Tang Shengjing, Shi Jiao. The application of thrust vector control technology on missile[J]. Winged Missiles Journal, 2010(12): 52-59. (in Chinese)
    [2]
    Xie Yongqiang, Li Shun, Zhou Xufeng, et al. The application analysis of thrust vector control systems of air to air missile [J]. Science Technology and Engineering, 2009,9(20): 6109-6113. (in Chinese)
    [3]
    Qian Xingfang, Lin Ruixiong, Zhao Yanan. Missile flight dynamics [M]. Beijing: Beijing Institute of Technology Press, 2000: 36-50. (in Chinese)
    [4]
    Mracek Curtis P, Ridgely D Brett. Optimal control solution for dual (tail and canard) controlled missiles //AIAA Guidance, Navigation, and Control Conference and Exhibit. Reno,USA: AIAA, 2006.
    [5]
    Ridgely D Brett, Lee Yung, Fanciullo Todd. Dual aero/propulsive missile control-optimal control and control allocation //AIAA Guidance, Navigation, and Control Conference and Exhibit. Reno,USA: AIAA, 2006.
    [6]
    Yang Lingyu, Shen Gongzhang. A new optimal control allocation method for aircraft with multiple control effectors //45th AIAA Aerospace Sciences Meeting and Exhibit. Reno,USA: AIAA, 2007.
    [7]
    Cui Yankai, Wang Zhigang. Aerodynamic and thrust vector complex controller design of over the shoulder air-to-air missile [J]. Journal of Astronautics, 2010, 31(4): 1100-1104. (in Chinese)
    [8]
    Yan Xunliang, Xu Min, Chen Shilu, et al. Compound control allocationstrategy for turning of vertical launch [J]. Journal of System Simulation, 2009, 21(24): 7878-7882. (in Chinese)
    [9]
    Guo Suofeng, Sheng Gongzhang, Wu Chengfu, et al. Advanced flight control system[M]. Beijing: China National Defence Industry Press, 2003: 257-263. (in Chinese)
    [10]
    Ai Er, Wang Yangyang, Qu Xiangju. An analysis on the combination of aero/thrust vector control surfaces [J]. Flight Dynamics, 2005, 23(4): 20-24. (in Chinese)
    [11]
    Feng Guohu, Zhang Dayong, Zhang Xinli, et al. Control allocation strategy for composite control of new unmanned-air vehicle[J]. Journal of Astronautics, 2008, 29(4): 1302-1307. (in Chinese)
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