contributor author | Ze Zhu | |
contributor author | Zhanxia Zhu | |
date accessioned | 2024-12-24T10:14:04Z | |
date available | 2024-12-24T10:14:04Z | |
date copyright | 11/1/2024 12:00:00 AM | |
date issued | 2024 | |
identifier other | JAEEEZ.ASENG-5258.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4298541 | |
description abstract | This paper proposes a saturation-optimized, quasi-sliding-mode model-free adaptive control (SM-MFAC) method to control the postcollision calming motion of an unstable free-flying space robot with saturated output torque. Initially, the dynamics model of the unstable free-flying space robot is transformed into a class of multiple-input, multiple-output (MIMO) discrete-time nonlinear systems. Here, the system characteristics can be estimated based on measured base attitude and joint angle data. The discrete sliding-mode control helps calculate the desired angular velocity at the current moment. Next, Hildreth’s method is used to introduce constraints to the control input criterion function for real-time tracking of the desired angular velocity, which enables the completion of the calming motion control of the free-flying space robot. The proposed algorithm simplifies the traditional calming motion control process by avoiding complex and redundant modeling requirements, ensuring that the control torque remains within predefined limits to optimize possible saturation. It also proves the convergence of the system output theoretically, and good stability and dynamic characteristics of the control scheme are verified through numerical simulations. | |
publisher | American Society of Civil Engineers | |
title | Saturation-Optimized Quasi-Sliding-Mode Calming Control of Free-Flying Space Robots Based on Model-Free Adaptive Control Theory | |
type | Journal Article | |
journal volume | 37 | |
journal issue | 6 | |
journal title | Journal of Aerospace Engineering | |
identifier doi | 10.1061/JAEEEZ.ASENG-5258 | |
journal fristpage | 04024087-1 | |
journal lastpage | 04024087-8 | |
page | 8 | |
tree | Journal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 006 | |
contenttype | Fulltext | |