中文摘要：

空间交会轨迹设计是交会任务的重要内容。文中分析了变轨过程中轨道执行精度误差和姿态控制精度误差对控制效果产生的影响，综合考虑了相位调节燃料消耗和交会终端精度问题，给出了一种交会任务中特征点和Lambert多脉冲联合控制方法。通过两组不同初始轨道参数的联合控制仿真算例验证了该方法的有效性。

英文摘要：

The trajectory design of space rendezvous is an important content in space rendezvous task. Execution error during orbit maneuver and influence of attitude control error are analyzed. By considering several factors including fuel consumption during phase adjustment and teminal precision, multi-impulse combination control design is proposed for rendezvous task. The validity is shown by two groups of different initial value simulations examples.