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基于尾流的超空泡航行体变结构制导律设计

李惠峰 张任天 宋佳

李惠峰, 张任天, 宋佳等 . 基于尾流的超空泡航行体变结构制导律设计[J]. 北京航空航天大学学报, 2012, 38(8): 987-991.
引用本文: 李惠峰, 张任天, 宋佳等 . 基于尾流的超空泡航行体变结构制导律设计[J]. 北京航空航天大学学报, 2012, 38(8): 987-991.
Li Huifeng, Zhang Rentian, Song Jiaet al. Novel sliding-mode guidance law for supercavitating vehicles based on wake information[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(8): 987-991. (in Chinese)
Citation: Li Huifeng, Zhang Rentian, Song Jiaet al. Novel sliding-mode guidance law for supercavitating vehicles based on wake information[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(8): 987-991. (in Chinese)

基于尾流的超空泡航行体变结构制导律设计

详细信息
  • 中图分类号: TJ 765

Novel sliding-mode guidance law for supercavitating vehicles based on wake information

  • 摘要: 针对超空泡航行体机动能力差、探测手段有限等特点,提出了一种基于目标舰船尾流梯度信息的变结构制导律.通过激光探测机动目标的尾流信息,动态解算尾流梯度方向;采用滑模变结构理论设计制导律,实现对尾流梯度方向的精确跟踪,最终完成对目标舰船的精确打击.该方法利用目标尾流信息,避免对目标运动状态进行复杂估计计算,不仅降低了对机动能力的要求,同时大大减小能量消耗,提高了有效航程.仿真结果表明,系统响应迅速,可以实现快速精确的目标跟踪打击,且具有很强的鲁棒性和抗干扰性.

     

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出版历程
  • 收稿日期:  2011-03-29
  • 网络出版日期:  2012-08-30

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