本文研究航天器利用气动力辅助变轨实现由远地轨道向近地轨道异面转移问题，就航天器利用大气飞行实现减速及轨道平面机动提出了一种考虑过程约束存在时的优化设计方法。通过方案设计将函数优化问题转换成参数优化问题，并利用美国航天飞机数据进行了模拟计算，得到满意结果。 In this paper, we study the spacecraft using aero-power-assisted orbit-changing to achieve the problem of surface-to-surface orbital transfer from the far-to-near-orbit to spacecraft, and propose an optimal design method that considers the constraints of the process when the spacecraft uses the atmospheric flight to achieve deceleration and orbital maneuvering. Through the program design, the function optimization problem is transformed into the parameter optimization problem, and the simulation results are obtained by using the data of the U.S. space shuttle.