The Model and Simulation of Transfer Alignment of Carrier based Aircraft INS with Large Azimuth Misalign Angle

摘要：

In order to solve the initial alignment problem of carrier based aircraft with a large azimuth misalignment condition, the error model of transfer alignment is built. This model transfers large azimuth misalignment angle problem between carrier coordinates and aircraft real coordinates into small azimuth misalignment angle problem between aircraft ideal coordinates and aircraft real coordinates, the linear error model is conducted and simulated via velocity matching method. The simulation result proves the validity and feasibility of the model.

作者: Qingwei Gao Guorong Zhao Xibing Wang

作者单位: Department of Command Naval Aeronautical & Astronautical University Yantai 264001, P.R.China Department of Control Engineering Naval Aeronautical & Astronautical University Yantai 264001, P.R.C

会议类型: 国际会议

会议名称: The Second International Joint Conference on Computational Science and Optimization(CSO 2009)(2009 国际计算科学与优化会议)

会议地点: 三亚

会议语种:英文

页码: 355-358

在线出版日期: 2009-04-24（万方平台首次上网日期，不代表论文的发表时间）