Multi-pulse Maneuver Orbit Optimization based on a new hybrid algorithm
For the Lambert method based on two-body supposition and do not account for actual orbit perturbation affection, we put forward a new orbit maneuver optimization method which suits for an arbitrary number impulse maneuver accounting for perturbation affection. Firstly, we describe the maneuver process by equation accounting for perturbation affection. Then we combine the equation with nonlinear programming with constraints and get a set of optima equations. Thirdly, we use a new hybrid algorithm to solve the optimal problem, which combine SQP with PSO and can reinforces the search accuracy and improves the convergence. Finally, the simulation results show that this method is feasible and can be used to solve multi-impulse perturbation orbit transform problem efficiently.
Multi-pulse orbit maneuver perturbation affection Nonlinear programming with constraints
Li Chunks
College of Astronautics Northwestern Polytechnical University Youyi Road, Xian, 710072,China
国际会议
厦门
英文
577-580
2010-10-29(万方平台首次上网日期,不代表论文的发表时间)