4.7 Article

3D Soft-Landing Dynamic Theoretical Model of Legged Lander: Modeling and Analysis

期刊

AEROSPACE
卷 10, 期 9, 页码 -

出版社

MDPI
DOI: 10.3390/aerospace10090811

关键词

legged lander; soft landing; dynamic modeling; dynamic analysis; contact and friction model

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This paper presents a novel 3D soft-landing dynamic model for a legged lander and its numerical solution process. The model takes into account the 6-DOF motion of the lander's base model with mass center offset settings, as well as the 3-DOF spatial motion of each landing gear. The model also considers factors such as buffering force, footpad-ground contact, and inter-structure friction. Comparative studies with a simulated model validate the proposed model's effectiveness, and further investigation into different contact force and friction models provide insights into the soft-landing performance of the lander.
In this paper, a novel 3D (three-dimensional) soft-landing dynamic theoretical model of a legged lander is developed in detail as well as its numerical solution process. The six degrees of freedom motion (6-DOF) of the base model of the lander with mass center offset setting is considered in the model as well as the spatial motion (3-DOF) of each landing gear. The characteristics of the buffering force, the footpad-ground contact, and the inter-structure friction are also taken into account during the motion of each landing gear. The direct constraint violation correction is used to control the constraint stabilization of the nonlinear dynamic equation. Comparative studies between the results from the proposed model and the simulated model (built in MSC Adams) under four classical load cases show the validity of the model. Additionally, the influences of different types of contact force models, friction force models, and a friction correction model used in the soft-landing dynamic model are further investigated as a step toward understanding the soft-landing dynamic performance and the feasibility of the dynamic model method of a legged lander. The results indicate that a precise lateral force model of the footpad-ground contact is necessary to obtain the soft-landing performance of one lander during soft landing.

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