Conceptual design and analysis of legged landers with orientation capability  

作　　者：Rongfu LIN Weizhong GUO Changjie ZHAO Mingda HE 

机构地区：[1]State Key Laboratory of Mechanical System and Vibration,School of Mechanical Engineering,Shanghai Jiao Tong University,200240,China

出　　处：《Chinese Journal of Aeronautics》2023年第3期171-183,共13页中国航空学报（英文版）

基　　金：partial financial support under the projects from the National Natural Science Foundation of China(Nos.51735009 and 51905338);the State Key Laboratory of Mechanical System and Vibration,China(No.MSVZD-2016-08);the China Postdoctoral Science Foundation(No.2019M651487)。

摘　　要：The lander with orientation capability is of fundamental importance for the“Returning”mission because its body can be the base with a suitable launching angle for the ascender lifting off.This paper proposes the conceptual design and verification of Landers with Orientation Capability(LOCs).Firstly,the topological composition of the lander is analyzed and expressed in the form of Lie group,which provides the fundamental principle for the type synthesis of LOCs.Then,the type synthesis approach for designing LOCs is proposed,which includes designing the Equivalent Parallel Mechanism(EPM)and the auxiliary limbs.Numerous mechanisms of LOCs with twodimensional rotational motions are obtained based on the type synthesis approach by developing and combining the EPMs and auxiliary limbs.Afterward,kinematics and Jacobian matrix of a typical legged lander are developed,the workspace is analyzed,singularity configurations are analyzed based on the wrench graph method,and finally,the orientation capability is analyzed.The pitch and yaw angle reach 17.5°,considering the permissible range of joints.The proposed types of LOCs offer potential candidate for the“Returning”mission of the exploration mission.

关 键 词：Legged lander Orientation analysis Orientation capability Parallel mechanism Type synthesis 

分 类 号：V423[航空宇航科学与技术—飞行器设计]