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In this paper, the design process of two robust H∞ control architectures for a Gun Launched Micro Aerial Vehicle — GLMAV — is presented. The process starts with the developement of a nonlinear dynamic model reflecting the important elements of the GLMAV. This model is then linearized around hover and used for the design of static output feedback H∞ controllers for position and orientation control...
This paper considers the problem of controlling the position and the orientation of a Gun Launched Micro Aerial Vehicle - GLMAV - despite unknown aerodynamic efforts. The proposed approach overcomes the problem of gyroscopic coupling by taking advantage from the structure of the thrust mechanism, which is made of two counter rotating propellers. An adaptive linearizing controller is designed, allowing...
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