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)

摘要

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.

原文English
頁(從 - 到)109-129
頁數21
期刊International Journal of Robust and Nonlinear Control
11
發行號2
DOIs
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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