This paper studies the multiple model adaptive estimator (MMAE) for nonlinear systems with unknown disturbances. Multiple models are constructed with a set of process noise covariance matrices, such that the algorithm that consists of multiple parallel filters can adapt to different levels of unknown disturbances. The filtering stability of the MMAE is analyzed for the considered system. Sufficient conditions to ensure the boundedness of the algorithm is provided. Then we focus on the utilization of the MMAE for spacecraft relative navigation missions. The ability to know precise position of a space target is critical to mission planners for reaching science objectives as well as avoiding catastrophic collisions with other spacecrafts or space debris. In order to improve the observability of the system, the double LOS measuring target tracking technique is used. A performance comparison among an extended Kalman filter (EKF), a nonlinear robust filter (NRF) and the MMAE is carried out for spacecraft relative navigation, where the position of a space target is estimated by using double line-of-sight (LOS) measurements. Simulation studies illustrate that the MMAE performs better than the EKF and the NRF.
XIONG Kai ,WEI Chunling.
SPACECRAFT RELATIVE NAVIGATION BASED ON MULTIPLE MODEL ADAPTIVE ESTIMATOR. Journal of Systems Science and Mathematical Sciences, 2014, 34(7): 828-837 https://doi.org/10.12341/jssms12378