Hierarchical Passivity-Based Force-Position-Configuration Coordinated Control of Multi-Branch Spacecraft

IF 5.7 2区 计算机科学 Q1 ENGINEERING, AEROSPACE IEEE Transactions on Aerospace and Electronic Systems Pub Date : 2024-11-18 DOI:10.1109/TAES.2024.3499911
Lang Lu;Chengfei Yue;Qiang Shen;Xibin Cao
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Abstract

The multibranch spacecraft have attracted significant attention owing to their exceptional dexterity, extensive operational range, and capability to independently or collaboratively execute diverse space tasks. The control target of this kind of spacecraft mainly lies in two levels, i.e., precise force/position control of the arm end-effector with adaptivity to the environment and configuration maintenance control of the whole body with guaranteed stability. This article focuses on the whole-body coordination and compliance control of redundant multibranch spacecraft in the space station surface manipulation scenario, and proposes a hierarchical passivity-based force-position-configuration multilevel coordinated control framework. In the proposed framework, the leader–follower cooperative strategy is used to generate the desired positions and attitude of the end-effector; the hierarchical passive control structure based on the null space is utilized to enable multilevel compatible control; the adaptive variable impedance control strategy is embedded in the end-effector compliance control level to achieve safe and compliant contact on the target; the passive compensation control of the multiarm spacecraft system based on the energy tank is added in each control level to ensure the safety and stability of the system operation process. Finally, the efficacy of the proposed control framework is demonstrated through formal proofs and simulation results.
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基于分层被动性的多分支航天器力-位置-配置协调控制
多分支航天器由于其特殊的灵活性、广泛的操作范围以及独立或协同执行各种空间任务的能力而引起了极大的关注。这类航天器的控制目标主要在于两个层面,即具有环境适应性的臂端执行器的精确力/位置控制和保证稳定性的整体构型保持控制。针对空间站表面操纵场景下冗余多分支航天器的全身协调与柔度控制问题,提出了一种基于分层无源的力-位置-位姿多级协调控制框架。在该框架中,采用领导-追随者合作策略生成末端执行器的期望位置和姿态;采用基于零空间的分层被动控制结构,实现多级兼容控制;在末端执行器柔度控制层嵌入自适应变阻抗控制策略,实现与目标的安全柔度接触;为保证系统运行过程的安全稳定,在各控制层增加了基于能量罐的多臂航天器系统的无源补偿控制。最后,通过形式证明和仿真结果验证了所提控制框架的有效性。
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来源期刊
CiteScore
7.80
自引率
13.60%
发文量
433
审稿时长
8.7 months
期刊介绍: IEEE Transactions on Aerospace and Electronic Systems focuses on the organization, design, development, integration, and operation of complex systems for space, air, ocean, or ground environment. These systems include, but are not limited to, navigation, avionics, spacecraft, aerospace power, radar, sonar, telemetry, defense, transportation, automated testing, and command and control.
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