联结翼无人机着舰性能分析  

Analysis on Carrier Landing Performance of the Joined-Wing UAV

作　　者：郭卫刚 李涛 GUO Weigang;LI Tao(Naval Aviation University,Yantai Shandong 264001,China;Naval 4808 Ordnance Repair Factory,Qingdao Shandong 266044,China)

机构地区：[1]海军航空大学,山东烟台264001 [2]海军4808军械修理厂,山东青岛266044

出　　处：《海军航空工程学院学报》2018年第4期418-422,共5页Journal of Naval Aeronautical and Astronautical University

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。The joined-wing UAV has the characteristics of large lift, good controllability and stability. In order to participate in the UAV race, a joined-wing configuration UAV ,was designed. It could takeoff, throw, waveoff arrested deck-landing 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.

关 键 词：无人机 试飞 联接翼 飞行性能 

分 类 号：V221[航空宇航科学与技术—飞行器设计]