Algorithmization of Guidance and Motion Control of a Space Manipulation Robot in the Service Tasks of a Non-Operative Spacecraft

Q4 Engineering
N. Kozlova, A. Fomichev
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引用次数: 0

Abstract

Nowadays there are many non-functioning spacecraft in orbit that have run out of fuel, or have failed due to breakdown. Therefore, the concept of a serviced space and the development of space manipulation robot for extending the spacecraft service life are becoming expedient. Space manipulation robot will be able to perform a variety of tasks, from inspecting malfunctions of a serviced spacecraft, to performing repairs and refueling the target vehicle. The article proposes a strategy and algorithms for the guidance and motion control of a space manipulation robot at the stage of rendezvous with a non-cooperative spacecraft to perform maintenance tasks. The purpose of the article is to synthesize the control of the translational and rotational motion of the space manipulation robot for its convergence with the target satellite at a given distance. The control system is presented in the form of a hierarchical two-level "guidance-stabilization" system. At the guidance level, a transition quaternion of the associated coordinate system to the required position is formed, as well as thrust engine control, which ensures the translational motion of the space manipulation robot at the required velocity. At the stabilization level, a control is formed that superpose the associated coordinate system of the space manipulation robot with the direction to the served satellite. The article proposes a scheme and a mathematical model of the propulsion system, angular and translational motion of the service satellite. The modeling of the developed guidance and motion control algorithms in the SIMULINK environment has been carried out.
非操作航天器服务任务中空间操作机器人的制导与运动控制算法
如今,轨道上有许多因燃料耗尽或故障而无法运行的航天器。因此,服务空间的概念和空间操纵机器人的发展是延长航天器使用寿命的有利条件。空间操纵机器人将能够执行各种任务,从检查服务航天器的故障,到执行维修和为目标飞行器加油。提出了一种空间操纵机器人在与非合作航天器交会阶段执行维修任务的制导和运动控制策略和算法。本文的目的是综合控制空间操纵机器人的平移运动和旋转运动,使其在给定距离上与目标卫星收敛。该控制系统以分层两级“制导-镇定”系统的形式提出。在制导层形成关联坐标系到所需位置的过渡四元数,并进行推力发动机控制,保证空间操纵机器人在所需速度下的平移运动。在稳定层,将空间操纵机器人的关联坐标系与所服务卫星的方向进行叠加,形成控制。本文提出了业务卫星推进系统、角运动和平移运动的方案和数学模型。在SIMULINK环境下对所开发的制导和运动控制算法进行了建模。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Mekhatronika, Avtomatizatsiya, Upravlenie
Mekhatronika, Avtomatizatsiya, Upravlenie Engineering-Electrical and Electronic Engineering
CiteScore
0.90
自引率
0.00%
发文量
68
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