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高超声速飞行器抗干扰反步滑模控制

后德龙 王青 王通 董朝阳

后德龙, 王青, 王通, 等 . 高超声速飞行器抗干扰反步滑模控制[J]. 北京航空航天大学学报, 2014, 40(1): 80-85.
引用本文: 后德龙, 王青, 王通, 等 . 高超声速飞行器抗干扰反步滑模控制[J]. 北京航空航天大学学报, 2014, 40(1): 80-85.
Hou Delong, Wang Qing, Wang Tong, et al. Disturbance rejection sliding mode control of hypersonic vehicle based on backstepping method[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(1): 80-85. (in Chinese)
Citation: Hou Delong, Wang Qing, Wang Tong, et al. Disturbance rejection sliding mode control of hypersonic vehicle based on backstepping method[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(1): 80-85. (in Chinese)

高超声速飞行器抗干扰反步滑模控制

基金项目: 国家自然科学基金资助项目(61074027,61273083)
详细信息
  • 中图分类号: TP273

Disturbance rejection sliding mode control of hypersonic vehicle based on backstepping method

  • 摘要: 针对存在参数不确定及外部扰动下的高超声速飞行器轨迹跟踪控制问题,研究了一种基于反步法的抗干扰滑模控制设计方法.将非线性高超声速飞行器动力学模型表达为严反馈形式分步进行设计.采用滑模控制方法进行每步的控制器设计,并提出采用扩展状态观测器(ESO,Extended State Observer)方法实现对参数不确定及外部扰动产生的内外干扰进行估计,继而在控制中补偿.扩展状态观测器能保证对干扰的估计收敛到真值附近的邻域内,从而能够保证较好的补偿效果.通过0.5°附加干扰攻角和25%的气动参数偏差下的非线性高超声速飞行器动力学模型仿真结果验证了该抗干扰滑模控制方案对内外干扰的抑制效果和闭环系统良好的跟踪性能.

     

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    [3] 黄显林, 葛东明.吸气式高超声速飞行器纵向机动飞行的鲁棒线性变参数控制[J].宇航学报, 2010, 31(7):1789-1796 Huang Xianlin, Ge Dongming.Robust parameter-varying control for longitudinal maneuvering flight of air-breathing hypersonic vehicle[J].Journal of Astronautics, 2010, 31(7):1789-1796(in Chinese)
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出版历程
  • 收稿日期:  2013-03-15
  • 网络出版日期:  2014-01-20

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