Three-dimensional nonlinear H guidance law

Ciann Dong Yang, Hsin Yuan Chen

研究成果: Article同行評審

35 引文 斯高帕斯(Scopus)


This paper proposes a novel three-dimensional missile guidance law design based on nonlinear H control. The complete nonlinear kinematics of pursuit-evasion motion is considered in the three-dimensional spherical co-ordinates system; neither linearization nor small angle assumption is made here. The nonlinear H guidance law is expressed in a simple form by solving the associated Hamilton-Jacobi partial differential inequality analytically. Unlike adaptive guidance laws, the implement of the proposed robust H guidance law does not require the information of target acceleration, while ensuring acceptable interceptive performance for arbitrary target with finite acceleration. The resulting pursuit-evasion trajectories for both the H-guided missile and the worst-case target are determined in closed form, and the performance robustness against variations in target acceleration, in engagement condition, and in control loop gain, is verified by numerical simulations.

頁(從 - 到)109-129
期刊International Journal of Robust and Nonlinear Control
出版狀態Published - 2001 一月 1

All Science Journal Classification (ASJC) codes

  • 控制與系統工程
  • 化學工程 (全部)
  • 生物醫學工程
  • 航空工程
  • 機械工業
  • 工業與製造工程
  • 電氣與電子工程


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