{"title":"Contact dynamics and force control of space manipulator systems","authors":"S. W. Kim, A. Misra, V. Modi","doi":"10.1098/rsta.2001.0886","DOIUrl":null,"url":null,"abstract":"Detailed modelling of contact dynamics involving a flexible space manipulator system and a payload is considered in this paper. The components undergoing direct contact (the end–effector of a manipulator and a payload) are modelled using the finite–element method, while the rest of the system is handled through the usual flexible multi–body formulation. Then, the system dynamics is composed of a set of differential equations subjected to sets of algebraic equations expressing kinematic or contact constraints. This dynamic model is then used to design a composite controller which must simultaneously achieve three goals: (i) trajectory tracking, (ii) force control and (iii) stabilization of the flexible degrees of freedom of the multi–body system. The singular perturbation method is used to obtain two reduced–order models; subsequently, the slow subsystem is used to design a hybrid position/force controller based on impedance control, and the fast subsystem is used to design a linear quadratic regulator (LQR).","PeriodicalId":20023,"journal":{"name":"Philosophical Transactions of the Royal Society of London. Series A, Mathematical and Physical Sciences","volume":"17 1","pages":"2271 - 2286"},"PeriodicalIF":0.0000,"publicationDate":"2001-11-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"3","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Philosophical Transactions of the Royal Society of London. Series A, Mathematical and Physical Sciences","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1098/rsta.2001.0886","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 3
Abstract
Detailed modelling of contact dynamics involving a flexible space manipulator system and a payload is considered in this paper. The components undergoing direct contact (the end–effector of a manipulator and a payload) are modelled using the finite–element method, while the rest of the system is handled through the usual flexible multi–body formulation. Then, the system dynamics is composed of a set of differential equations subjected to sets of algebraic equations expressing kinematic or contact constraints. This dynamic model is then used to design a composite controller which must simultaneously achieve three goals: (i) trajectory tracking, (ii) force control and (iii) stabilization of the flexible degrees of freedom of the multi–body system. The singular perturbation method is used to obtain two reduced–order models; subsequently, the slow subsystem is used to design a hybrid position/force controller based on impedance control, and the fast subsystem is used to design a linear quadratic regulator (LQR).