... in the field of aerospace. This paper aims at analyzing and simulating the RRD in target orbit for maneuvering spacecrafts with a single fixed-magnitude impulse and continuous thrust, respectively, to provide a basis for analyzing the feasibility of spacecraft maneuvering missions and improving the design...

... Kalman filter (EKF)-based on-line orbit determination method with continuous thrust acceleration. Weichao et al. (2013) proposed an unscented Kalman filter-based estimation algorithm for mean orbital elements in autonomous satellite guidance and orbit control. It is worth noting that the above...