Kalman/Particle Filter for Integrated Navigation System
Particlc filter is introduced.Since the particle filter would bring hard computation,a new Kalman/Particle mixed filter used on SINS/GPS integrated navigation system was proposed.The new method divides the system into two submodels,one is linear,the othcr one is nonlinear,and then implement Kalman filter and particle filter separately.The simulation results show that their performance is almost equal,but the computation complexity of the Kalman/particle filter is much lower than traditional praticle filter.
integrated navigation system particle filter kalman/partcle filter
Zhun Jiao Rong Zhang
Department of Aerial Instnunent and Electric Engineering The First Aviation College of Air Force Xin Air Force Engineering University Xian, China
国际会议
太原
英文
966-969
2012-12-08（万方平台首次上网日期，不代表论文的发表时间）