Observability Analysis and Simulation of Integrated Navigation System During Maneuver
An observability analysis of SINS/GPS is presented based on perturbation model with respect to the local level frame. Linear acceleration and constant angular rate are chosen as maneuver mode during the observability analysis. Rank condition of Observability matrix and singular value decomposition were used as the analysis method. Under the same maneuver condition and simulation condition, the analysis results were compared, the recommendation was finally given to enhance the observability of integrated navigation system and convergence of data fusion system.
LIU Zhiping YU Fan
School of Computer Science and Engineering, Xi’an Technological University, Xi’an 710032, P.R.Chian
国际会议
The 30th Chinese Control Conference(第三十届中国控制会议)
烟台
英文
1-4
2011-07-01（万方平台首次上网日期，不代表论文的发表时间）