Observer-Based Optimal Zero-Sliding Midcourse Guidance for Missiles with TVC and DCS

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概要

• 論文の詳細を見る
• 2013-01-04

著者

• YEH Fu-Kuang

  Department of Aviation Electronics, China University of Science and Technology

• KOU Kuang-Yang

  Department of Traffic Science, National Central Police University

関連論文

• Sliding-Mode Controller Design for a Mini-UAV with Propellers
• Observer-Based Optimal Zero-Sliding Midcourse Guidance for Missiles with TVC and DCS
• Observer-Based Optimal Zero-Sliding Midcourse Guidance for Missiles with TVC and DCS

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