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专利摘要显示,本公开是关于一种飞行路径信息的上报方法及装置、信息确定方法及装置、基站、无人机和计算机可读存储介质
来源:1.北京航空航天大学 无人系统研究院,2.北京航空航天大学 航空科学与工程学院 | 作者:向锦武,阚 梓,邵浩原,李华东,董 鑫,李道春 | 发布时间: 2021-07-14 | 38041 次浏览 | 分享到:
对长航时无人机的发展现状及关键技术进行了分析与总结.长航时无人机留空时间长,作业覆盖区域广....

[147]WANG Rui, ZHU Xiaoping, ZHOU Zhou. Design gust alleviation controller for highly flexible solar UAV[C]//Proceedings of the 3rd International Conference on Measuring Technology and Mechatronics Automation. Shangshai: IEEE, 2011: 930. DOI: 10.1109/ICMTMA. 2011.233

[148]COOK R G, PALACIOS R, GOULART P. Robust gust alleviation and stabilization of very Flexible Aircraft[J]. AIAA Journal, 2013, 51(2): 330. DOI: 10.2514/1.J051697

[149]WANG Yinan, WYNN A, PALACIOS R. Nonlinear modal aeroservoelastic analysis framework for flexible aircraft[J]. AIAA Journal, 2016, 54(10): 3075. DOI: 10.2514/1.J054537

[150]ZENG Jie, MOULIN B, BRENNER M J. Adaptive feedforward control for gust load alleviation[J]. Journal of Guidance Control and Dynamics, 2010, 33(3): 862. DOI: 10.2514/1.46091

[151]陈磊, 吴志刚, 杨超, 等. 多控制面机翼阵风减缓主动控制与风洞试验验证[J]. 航空学报, 2009, 30(12): 2250

CHEN Lei, WU Zhigang, YANG Chao, et al. Active control and wind tunnel test verification of multi-control surfaces wing for gust alleviation[J]. Acta Aeronautica et Astronautica Sinica, 2009, 30(12): 2250

[152]GADIENT R, LAVRETSKY E, WISE K. Very flexible aircraft control challenge problem[C]//Proceedings of the AIAA Guidance, Navigation, and Control Conference. Minneapolis, Minnesota: AIAA, 2012: 1. DOI: 10.2514/6.2012-4973

[153]HAGHIGHAT S, LIU H, MARTINS J. Mixed-norm multi-objective robust controller applied to a very flexible aircraft[C]//Proceedings of the AIAA Guidance, Navigation, and Control Conference. Portland, Oregon: AIAA, 2011: 1. DOI: 10.2514/6.2011-6256

[154]CHE Jiaxing, GREGORY I M, CAO Chengyu. Integrated flight/structural mode control for very flexible aircraft using l1 adaptive output feedback controller[C]//Proceedings of the AIAA Guidance, Navigation, and Control Conference. Minneapolis, Minnesota: AIAA, 2012: 1. DOI: 10.2514/6.2012-4439

[155]SHEARER C M, CESNIK C E S. Nonlinear flight dynamics of very flexible aircraft[J]. Journal of Aircraft, 2007, 44(5): 1528. DOI: 10.2514/1.27606

[156]ZHENG Qu, ANNASWAMY A M, LAVRETSKY E. Adaptive output-feedback control for a class of multi-input-multi-output plants with applications to very flexible aircraft[C]//Proceedings of the American Control Conference. Boston, MA: IEEE, 2016: 1613. DOI: 10.1109/ACC.2016.7525147