一种新型卫星对接环的对接装置设计与分析  

Design and Analysis of A New Docking Device for Satellite Docking Ring

作　　者：高碧祥 杨臻[1] 曲普[1] 黄剑斌[2] 

机构地区：[1]中北大学机电工程学院,山西太原030051 [2]中国空间技术研究院,北京100094

出　　处：《机械传动》2016年第11期123-126,共4页Journal of Mechanical Transmission

摘　　要：针对某种特殊结构的卫星的在轨服务任务下提出的技术要求,介绍了一种基于凸轮曲线机构及连杆机构的对接装置,可以实现对目标星对接环的特殊对接技术要求,且装置结构成熟、锁紧力大、运动平稳。以对接装置的凸轮曲线从动件的数学模型和三维实体模型为基础,通过Matlab和ADAMS软件分别进行运动规律的求解和仿真,将得到的对接装置的理论及仿真运动数据进行对比,验证了该对接装置能完成既定的设计目标。For a particular structure satellite, under the proposed requirements of on - orbit service task technical, a kind of docking device based on CAM curve mechanism and linkage mechanism is introduced, which can achieve the special docking technology requirement of the target satellite docking ring. And the device is mature structure, large clamping force and smooth movement. Based on the mathematical model of docking device cam curve follower and 3 D entity model, the motion law of mathematical model and 3 D model are respectively solved and simulated by Matlab and ADAMS software. Then comparing the docking device theory and simulation of motion data to verify the docking device could complete the design of the goal.

关 键 词：卫星对接环 对接装置 数学模型 求解与仿真 运动规律 

分 类 号：V423.4[航空宇航科学与技术—飞行器设计]