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作 者:李婧婷 邢振林 张雷[3] 董一群 艾剑良 LI Jingting;XING Zhenlin;ZHANG Lei;DONG Yiqun;AI Jianliang(Shanghai Aerospace Equipments Manufacturer Co.Ltd.,Shanghai 200000,China;Department of Aeronautics and Astronautics Fudan University,Shanghai 200000,China;Shenyang Aircraft Design and Research Institute AVIC,Shenyang 110000,China)
机构地区:[1]上海航天设备制造总厂有限公司,上海200000 [2]复旦大学航空航天系,上海200000 [3]沈阳飞机设计研究所,沈阳110000
出 处:《电光与控制》2023年第7期40-45,共6页Electronics Optics & Control
摘 要:针对舰载机无人机协同起降场景给出了舰载无人机编队起飞、返航过程中的任务剖面。提出了各飞行阶段的航线设计要求,对起飞等待阶段、进近等待阶段、下滑着舰阶段以及复飞等待阶段的舰载无人机飞行航线分别进行了设计,得到舰载无人机编队自主协同起降的全过程飞行航线及其相应的飞行关键点。最终,通过Matlab对所设计的航线进行了仿真验证,仿真结果验证了所设计的飞行航线符合相应的设计要求。Aiming at the cooperative take-off and landing scenarios of carrier-based UAV,the mission profile of carrier-based UAV formation during take-off and return is given.The flight route design requirements of each flight stage are put forward,and the flight routes of carrier-based UAVs in take-off waiting stage,approach waiting stage,landing stage and wave-off waiting stage are designed respectively,and the whole flight route of autonomous cooperative take-off and landing of carrier-based UAV formation and its corresponding flight key points are obtained.Finally,the designed flight route is simulated and verified by Matlab,and the simulation results verify that the designed flight route meets the corresponding design requirements.
分 类 号:V249[航空宇航科学与技术—飞行器设计]
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