| 联结翼无人机着舰性能分析 |
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| 引用本文： | 郭卫刚,李涛.联结翼无人机着舰性能分析[J].海军航空工程学院学报,2018,33(4):418-422. |
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| 作者姓名： | 郭卫刚 李涛 |
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| 作者单位： | 海军航空大学;海军4808军械修理厂 |
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| 摘 要： | 联结翼无人机具有升力大,操稳性好等特点。文章设计了一种联结翼无人机,可以模拟舰载机完成起飞、任务投掷、触舰复飞、在移动甲板上拦阻着舰等任务。通过控制方式和导引方式的优化组合,并考虑无人机飞行动力特点及运动方式进行试飞分析,结果表明:无人机的飞行性能、操稳性能及对指令的跟随性能都达到满意的效果,可为大型无人机上舰提供理论基础和技术支持。
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| 关 键 词： | 无人机 试飞 联接翼 飞行性能 |
Analysis on Carrier Landing Performance of the Joined-Wing UAV |
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| GUO Weigang and LI Tao.Analysis on Carrier Landing Performance of the Joined-Wing UAV[J].Journal of Naval Aeronautical Engineering Institute,2018,33(4):418-422. |
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| Authors: | GUO Weigang and LI Tao |
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| Institution: | Naval Aviation University, Yantai Shandong 264001, China and Naval 4808 Ordnance Repair Factory, Qingdao Shandong 266044, China |
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| Abstract: | The joined-wing UAV has the characteristics of large lift, good controllability and stability. In order to partici.pate in the UAV race, a joined-wing configuration UAV was designed. It could takeoff, throw, waveoff, arrested deck-land.ing which simulated carrier-based aircraft. With the constantly optimization of control, guide mode and flight dynamics,satisfied effect was obtained of the flight performance, controllability and stability and following quality for instructions.The results can provide the base of theory and support of technology for large carrier-based UAV. |
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| Keywords: | UAV flight test joined-wing flight performance |
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