Gong-Bo Wang · Yun-He Meng · Wei Zheng · Guo-Jian Tang College of Aerospace and Material Engineering,National University of Defense Technology,410073 Changsha,China
Abstract:
Sun synchronous orbit and frozen orbit formed due to J 2 perturbation have very strict constraints on orbital parameters,which have restricted the application a lot.In this paper,several control strategies were illustrated to realize Sun synchronous frozen orbit with arbitrary orbital elements using continuous low-thrust.Firstly,according to mean element method,the averaged rate of change of the orbital elements,originating from disturbing constant accelerations over one orbital period,was derived from Gaus...