摘要
研究了机载光电/惯性组合着舰导引新算法,综合光电探测系统获得的跑道成像信息和机载惯性导航信息,建立导引参数与成像信息之间的数学模型,利用最小二乘法估计舰/机相对位姿,补偿舰船纵摇、横摇及沉浮运动并预测舰载机着舰位置,以实现近程导引舰载机半自动或自动安全着舰。在算法研究的基础上,进行了地面车载验证实验。实验采用缩比方案,以着降跑道模拟器模拟运动中的着降跑道。试验车模拟舰载机,通过相对位姿关系的一致性模拟着舰过程。试验结果验证了着舰导引系统方案的可行性和有效性,为飞行实验奠定技术基础,有利于提高其安全性。
A new algorithm of aircraft carrier landing was studied utilizing airborne infrared camera/inertial integrated system, aiming to provide the guidance information and accomplish aircrafts semi-auto or auto landing. The mathematic relationship between guidance parameters and imaging information was modeled, and the relative position and attitude information between the carrier and the aircraft were estimated through least square method. Then the pitch, roll and heave movement of the carrier were compensated, so the touchdown point could be predicted in order to guide aircraft landing. Based on the theoretical research, the field verification tests were carried out, which adopted the minification scheme to simulate the process of aircraft carrier landing. In the experiments, the runway simulator simulated the motion of the carrier deck and the land vehicle was used as the aircraft. The results verify that the landing guidance system scheme is feasible and effective, and lays the technical foundation for the flight test and improves its safety.
出处
《中国惯性技术学报》
EI
CSCD
北大核心
2012年第2期178-182,共5页
Journal of Chinese Inertial Technology
基金
中航工业产学研合作创新基金(CXY2010BH04)
关键词
舰载机
红外探测
惯性导航
着舰
地面验证实验
carrier-based aircraft
infrared detecting
inertial navigation
carrier landing
field verification test
