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作 者:Tongyan Wu Yimin Deng Dukun Xu Baitao Zhu Xuanhe Xiang
出 处:《Guidance, Navigation and Control》2024年第2期194-200,共7页制导、导航与控制(英文)
基 金:supported by the National Natural Science Foundation of China under Grant Nos.62350048,T2121003 and U20B2071.
摘 要:Fixed-wing unmanned aerial vehicles(UAVs)are a primary focus of current UAV research.Challenges arise in theirflight due to high speed and complex maneuverability.This paper explores the coordinated turn guidance law for fixed-wing UAVs and validates an experimental leader-follower formation platform inflight.Results demonstrate the effectiveness of the proposed algorithm and platform in enabling actual leader-follower formationflights for fixed-wing UAVs.
关 键 词:Fixed-wing unmanned aerial vehicles guidance law flight experiment leaderfollower formation
分 类 号:V279[航空宇航科学与技术—飞行器设计] V249.3
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