Deprecated: $wgMWOAuthSharedUserIDs=false is deprecated, set $wgMWOAuthSharedUserIDs=true, $wgMWOAuthSharedUserSource='local' instead [Called from MediaWiki\HookContainer\HookContainer::run in /var/www/html/w/includes/HookContainer/HookContainer.php at line 135] in /var/www/html/w/includes/Debug/MWDebug.php on line 372
Analysis of load-carrying capacity for redundant free-floating space manipulators in trajectory tracking task - MaRDI portal

Analysis of load-carrying capacity for redundant free-floating space manipulators in trajectory tracking task (Q1717696)

From MaRDI portal





scientific article; zbMATH DE number 7015736
Language Label Description Also known as
English
Analysis of load-carrying capacity for redundant free-floating space manipulators in trajectory tracking task
scientific article; zbMATH DE number 7015736

    Statements

    Analysis of load-carrying capacity for redundant free-floating space manipulators in trajectory tracking task (English)
    0 references
    0 references
    0 references
    0 references
    0 references
    0 references
    8 February 2019
    0 references
    Summary: The aim of this paper is to analyze load-carrying capacity of redundant free-floating space manipulators (FFSM) in trajectory tracking task. Combined with the analysis of influential factors in load-carrying process, evaluation of maximum load-carrying capacity (MLCC) is described as multiconstrained nonlinear programming problem. An efficient algorithm based on repeated line search within discontinuous feasible region is presented to determine MLCC for a given trajectory of the end-effector and corresponding joint path. Then, considering the influence of MLCC caused by different initial configurations for the starting point of given trajectory, a kind of maximum payload initial configuration planning method is proposed by using PSO algorithm. Simulations are performed for a particular trajectory tracking task of the 7-DOF space manipulator, of which MLCC is evaluated quantitatively. By in-depth research of the simulation results, significant gap between the values of MLCC when using different initial configurations is analyzed, and the discontinuity of allowable load-carrying capacity is illustrated. The proposed analytical method can be taken as theoretical foundation of feasibility analysis, trajectory optimization, and optimal control of trajectory tracking task in on-orbit load-carrying operations.
    0 references

    Identifiers