加权
巡航控制
计算机科学
广义逆
包络线(雷达)
控制(管理)
控制理论(社会学)
控制工程
巡航导弹
反向
数学优化
工程类
数学
人工智能
航空航天工程
雷达
电信
医学
几何学
放射科
导弹
作者
Michael J. Acheson,Irene M. Gregory,Jacob Cook
摘要
View Video Presentation: https://doi.org/10.2514/6.2021-0999.vid Transition vehicles which combine vertical take off and landing with cruise configurations pose a unique challenge for control design and implementation. For this class of vehicle, successful control designs have historically broken the flight envelope into phases and modified the control approach for each phase. This research approaches control in a unified way across the entire envelope using a robust optimal design which provides effector weighting then implemented in a generalized Affine Generalized Inverse control allocation algorithm. System performance for a Lift plus Cruise transition vehicle is presented.
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