I-PD Flight Controller Design based on Integral-Type Optimal Servomechanism

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概要

• 論文の詳細を見る
• 2010-11-30

著者

• Ochi Yoshimasa

  Department Of Aerospace Engineering National Defense Academy

• KONDO Hiroyuki

  Graduate school of Science and Engineering, National Defense Academy

関連論文

• Missile Guidance Law Design via μ-Synthesis
• Design of a Ratio Servo Control System for a Toroidal CVT
• MIMO PID Controller Design Based on Integral-Type Optimal Servomechanism and Its Extension to Model-Following-Type
• I-PD Flight Controller Design based on Integral-Type Optimal Servomechanism

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