首页 | 本学科首页   官方微博 | 高级检索  
     

传递对准中载舰挠曲变形和杆臂效应一体化建模与仿真
引用本文:高青伟,赵国荣,王希彬,吴芳. 传递对准中载舰挠曲变形和杆臂效应一体化建模与仿真[J]. 航空学报, 2009, 30(11): 2172-2177
作者姓名:高青伟  赵国荣  王希彬  吴芳
作者单位:海军航空工程学院,指挥系,山东,烟台,264001;海军航空工程学院,控制工程系,山东,烟台,264001;海军航空工程学院,研究生管理大队,山东,烟台,264001
摘    要: 针对舰载机惯导系统大方位失准角传递对准的非线性问题,根据舰载机在载舰上的实际停放情况,引入舰载机标称坐标系,并综合考虑载舰挠曲变形和杆臂效应的影响,建立挠曲变形和杆臂效应加速度一体化模型,完善舰载机惯导系统大方位失准角传递对准线性化模型。采用“速度+角速度”组合匹配算法的滤波模型,对固定安装失准角和挠曲变形角进行了估计。结果表明,该模型在舰载机大方位失准角传递对准时可以满足对准精度和时间的要求。

关 键 词:传递对准  挠曲变形  杆臂效应  速度匹配  角速度匹配  惯性导航系统  初始对准

Incorporate Modeling and Simulation of Transfer Alignment with Flexure of Carrier and Lever-arm Effect
Gao Qingwei,Zhao Guorong,Wang Xibin,Wu Fang. Incorporate Modeling and Simulation of Transfer Alignment with Flexure of Carrier and Lever-arm Effect[J]. Acta Aeronautica et Astronautica Sinica, 2009, 30(11): 2172-2177
Authors:Gao Qingwei  Zhao Guorong  Wang Xibin  Wu Fang
Affiliation:1.Department of Command, Naval Aeronautical and Astronautical University2.Department of Control Engineering, Naval Aeronautical and Astronautical University3.Graduate Students’ Brigade, Naval Aeronautical and Astronautical University
Abstract:In order to solve the nonlinear transfer alignment problem for aircraft's inertial navigation system with large misalignment azimuth, an incorporate acceleration error model of lever-arm effect is built with the flexure of a carrier, and according to the actual position of the aircraft on the carrier, a linear error model of transfer alignment for aircraft's inertial navigation system with large misalignment azimuth is built and con-summated by importing nominal aircraft body coordinate. The velocity+angular velocity matching method is used to estimate both the fixed misalignment and the instantaneous dynamic distortion angle. The simulation result shows that this method can estimate the fixed misalignment and the flexure angle effectively, and satisfy the precision requirements.
Keywords:transfer alignment  flexure  lever-arm effect  velocity matching  angular velocity matching  inertial navigation systems  initial alignment
本文献已被 万方数据 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号