CAJ | 학술논문

某型高亚声速无人机连续出现两起飞行事故,在基本排除了机载设备故障的原因后,针对飞行控制失效的原因展开了深入的理论分析与飞控系统仿真试验,最终确定故障原因是在大飞行动压情况下,该型无人机控制参数出现不匹配.这为该型无人机以后的正常使用提供了理论依据,也为其他高速无人机的研制和使用提供了借鉴经验.采取相应改进措施后,后续该型无人机放飞取得成功.
모형고아성속무인궤련속출현량기비행사고,재기본배제료궤재설비고장적원인후,침대비행공제실효적원인전개료심입적이론분석여비공계통방진시험,최종학정고장원인시재대비행동압정황하,해형무인궤공제삼수출현불필배.저위해형무인궤이후적정상사용제공료이론의거,야위기타고속무인궤적연제화사용제공료차감경험.채취상응개진조시후,후속해형무인궤방비취득성공.
One type of subsonic unmanned aerial vehicles(UAVs) has continuously taken place two accidents. After eliminating the possibility of the equipment went blooey, the reason of the control action invalidation by theoretical analysis is searched and simulation. Finally, the reason is that the control parameters do not match under over much dynamic pressure. It provides a theoretical basis for normally use the type of UAV and experiences for developing other highspeed UAVs. By using the improved measures, the type of UAVs is more success for the subsequent flight.