• Infrared and Laser Engineering
  • Vol. 44, Issue 2, 693 (2015)
Li Yanhui*, Li Ming, Zhou Ling, and Zhang Nan
Author Affiliations
  • [in Chinese]
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    DOI: Cite this Article
    Li Yanhui, Li Ming, Zhou Ling, Zhang Nan. UAV flight controller design method based on model matching used for electro-optical reconnaissance[J]. Infrared and Laser Engineering, 2015, 44(2): 693 Copy Citation Text show less
    References

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    [3] Guo Suofeng, Shen Gongzhang. Advanced flight control system[M]. Beijing: National Defense Industry Press, 2003. (in Chinese)

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    [5] Pan Wei, Wang Xueyong, Jing Yuanwei. Mixed H2/H∞ state feedback controllers based on genetic algorithm[J]. Control and Decision, 2005, 20(2): 132-136. (in Chinese).

    [6] Li Guangwen. NGA based on uniform design and its application in optimization of FCS[J]. Acta Aeronautica ET Astronautica Sinica, 2008, 29: 73-78. (in Chinese)

    [7] Wang Yong. Lateral deviation correction control for UAV taxiing[J]. Acta Aeronautica ET Astronautica Sinica, 2008, 29: 142-149. (in Chinese)

    [8] Qian Xingfang, Lin Ruixiong, Zhao Yanan. Flight DynaIllic S0, Missile[M]. Beijing: Beijing Institute of Technology Press,2000. (in Chinese)

    [9] Li Ming. Hardware in closed loop simulation system for aircraft based on rapid simulation prototype[J]. Optics and Precision Engineering, 2008, 16: 1950-1955. (in Chinese)

    Li Yanhui, Li Ming, Zhou Ling, Zhang Nan. UAV flight controller design method based on model matching used for electro-optical reconnaissance[J]. Infrared and Laser Engineering, 2015, 44(2): 693
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