科技报告详细信息
Wing Shaping and Gust Load Controls of Flexible Aircraft: An LPV Approach
Hammerton, Jared R ; Su, Weihua ; Zhu, Guoming ; Swei, Sean Shan-Min
关键词: SHAPE OPTIMIZATION;    FLEXIBLE WINGS;    FLIGHT CONTROL;    FLIGHT CONDITIONS;    LINEAR PARAMETER-VARYING CONTROL;    AERODYNAMIC CONFIGURATIONS;    AERODYNAMIC LOADS;    CONTROL SURFACES;    GUST LOADS;    AIRFOILS;    COMPOSITE STRUCTURES;    MODELS;    AERODYNAMIC CHARACTERISTICS;   
RP-ID  :  ARC-E-DAA-TN50215
学科分类:航空航天科学
美国|英语
来源: NASA Technical Reports Server
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【 摘 要 】
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.
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