Motion Tracking Sliding-Mode Guidance of a Homing Missile with Bearings-Only Measurements

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概要

• 論文の詳細を見る

• Motion tracking sliding-mode control theory is utilized to design a homing-missile guidance law, which induces missile-target line-of-sight angular rate to track an arbitrarily given signal, such that observability for the target tracking with bearings-only measurements is enhanced. An adaptive two-step filter is used to estimate missile-target relative range, relative velocity, and target acceleration involved in the guidance law during the whole guidance period. Simulation studies indicate that the presented guidance law provides good performance for the filter, robustness to estimation errors, and good terminal effectiveness.

• 社団法人 日本航空宇宙学会の論文
• 2000-11-04

著者

• Zhou D

  Harbin Inst. Technol. Harbin Chn

• ZHOU Di

  Department of Control Science and Engineering, Harbin Institute of Technology

• MU Chundi

  Department of Automation, Tsinghua University

• Mu C

  Tsinghua Univ. Beijing Chn

• Mu Chundi

  Department Of Automation Tsinghua University

• Zhou Di

  Department Of Control Science And Engineering Harbin Institute Of Technology

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