In the proposed paper, the optimum wing shape of a highly flexible aircraft under varying flight conditions will be controlled by a linear parameter-varying approach. The optimum shape determined under multiple objectives, including flight performance, ride quality, and control effort, will be determined as well. This work is an extension of work done previously by the authors, and updates the existing optimization and utilizes the results to generate a robust flight controller.
Wing Shaping and Gust Load Controls of Flexible Aircraft: An LPV Approach
2018 AIAA SciTech Forum ; 2018 ; Kissimmee, FL, United States
2018-01-08
Conference paper
No indication
English
British Library Conference Proceedings | 2018
|Gust Load Alleviation System for BWB (Blended Wing Body) Flexible Aircraft
BASE | 2013
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