Simultaneous optimum design of shape and control system for micro air vehicles

Author:

Kajiwara Itsuro1,Haftka Raphael2

Affiliation:

1. Tokyo Inst. of Technology, Japan

2. Florida, Univ., Gainesville

Publisher

American Institute of Aeronautics and Astronautics

Cited by 7 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Control-oriented Design of Operating Range for Linear Parameter Varying Systems for Closed-Loop Performance;AIAA Guidance, Navigation, and Control Conference;2010-06-26

2. Simulator Development for Transition Flight Dynamics of a VTOL MAV;International Journal of Micro Air Vehicles;2010-06

3. Shape, Structure, and Kinematic Parameterization of a Power-Optimal Hovering Wing;51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 18th AIAA/ASME/AHS Adaptive Structures Conference<BR> 12th;2010-04-12

4. Automatic Control of VTOL Micro Air Vehicle During Transition Maneuver;AIAA Guidance, Navigation, and Control Conference;2009-06-14

5. Investigation of Flight Dynamics and Automatic Controls for Hovering Micro Air Vehicles;AIAA Guidance, Navigation and Control Conference and Exhibit;2008-06-15

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