Hypervelocity Trajectories of Ballistic Entry Using Improved Matched Asymptotic Expansions

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概要

• 論文の詳細を見る
• Japan Society for Aeronautical and Space Sciencesの論文
• 2000-02-04

著者

• Kuo Z‐s

  National Defense Univ. Twn

• Kuo Zeal-sain

  Department Of Mechanical Engineering Chung Cheng Institute Of Technology

• Yang Yuan-lung

  Department Of Mechanical Engineering Chung Cheng Institute Of Technology

• Kuo Zeql-Sain

  Department of Mechanical Engineering, Chung Cheng Institute of Technology

関連論文

• Dynamic Modeling and Analysis of Fixed-Wing Micro Air Vehicle
• Parameter Identification of Spin-Stabilized Projectiles Using a Modified Newton-Raphson Minimization Technique
• Hypervelocity Trajectories of Ballistic Entry Using Improved Matched Asymptotic Expansions
• Sliding-Mode Controller Design for a Mini-UAV with Propellers

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