Helicopter Flight Controller Design Using Nonlinear Transformation
スポンサーリンク
概要
著者
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OHTA Hirobumi
Department of Aeronautical Engineering, Nagoya University
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HAMIDI H.
Graduate School of Engineering, Nagoya University
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Hamidi H
Nagoya Univ. Nagoya Jpn
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Hamidi H.Ebneddin
Graduate School of Engineering, Nagoya University
関連論文
- A Complementary Flight Control System for Backside Landing
- Low Speed Turning Flight Path Control of a STOL Aircraft
- Effects of aerodynamics on a high-speed vehicle : aeroelastic analysis of the longitudinal motions
- Helicopter Flight Controller Design Using Nonlinear Transformation