基于递推二次规划算法的燃料最优有限推力远地点变轨

RQP Based Finite Thrust Apogee Orbit Transfer with Minimum Fuel

从工程实用的角度分析了静止通信卫星远地点变轨优化问题，定义了目标函数、约束条件及其相应的优化参数，根据问题特点，应用递推二次规划算法（RQP）进行变轨参数寻优，并用计算实例说明了此算法的有效性。

In the view of the engineering, analyses the optimal apogee orbit transfer for geostationary satellites and defines the objective function, constraint conditions and the optimized parameters. According to the nature of the problem, uses the RQP method to find the optimzed parameters in orbit transfer and demonstrates the validity of the method by an engineering example.