Force–Position Coordinated Compliance Control in the Adhesion/Detachment Process of Space Climbing Robot

Adhesion-based space climbing robots, with their flexibility and multi-functional capabilities, are seen as a promising candidate for in-orbit maintenance. However, challenges such as uncertain adhesion establishment, unexpected detachment, and body motion unsteadiness in microgravity environments persist. To address these issues, this paper proposes a coordinated force–position compliance control method that integrates novel adhesion establishment and rotational detachment strategies, integrated into the gait schedule for a space climbing robot. By monitoring the foot-end reaction forces in real time, the proposed method establishes adhesion without risking damaging the spacecraft exterior, and smooth detachment is achieved by rotating the foot joint instead of direct pulling. These strategies are dedicated to reducing unnecessary control actions and, accordingly, the required adhesion forces in all feet, reducing the possibility of unexpected detachment. Climbing experiments have been conducted in a suspension-based gravity compensation system to examine the merits of the proposed method. The experimental results demonstrate that the proposed rotational detaching method decreases the required pulling force by 65.5% compared to direct pulling, thus greatly reducing the disturbance introduced to the robot body and other supporting legs. When stepping on an obstacle, the compliant control method is shown to reduce unnecessarily aggressive control actions and result in a reduction in relevant normal and shear adhesion forces in the supporting legs by 44.8% and 35.1%, respectively, compared to a PID controller.

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Publication Details

Journal
Aerospace
Published
2024-12-31
DOI
https://doi.org/10.3390/aerospace12010020
Citations
2
Primary Topic
Space Satellite Systems and Control
Type
article
Field-Weighted Citation Impact
2.60

Funders

Controls
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article

Force–Position Coordinated Compliance Control in the Adhesion/Detachment Process of Space Climbing Robot

Pengfei Zheng, Changming Wen, Chao Chen, Chongbin Guo et al.
2 citations
Aerospace
Space Satellite Systems and Control
2.60
article

Force–Position Coordinated Compliance Control in the Adhesion/Detachment Process of Space Climbing Robot

Pengfei Zheng, Changming Wen, Chao Chen, Chongbin Guo, Zhenhao Jing
article en
2 citations

Abstract

Adhesion-based space climbing robots, with their flexibility and multi-functional capabilities, are seen as a promising candidate for in-orbit maintenance. However, challenges such as uncertain adhesion establishment, unexpected detachment, and body motion unsteadiness in microgravity environments persist. To address these issues, this paper proposes a coordinated force–position compliance control method that integrates novel adhesion establishment and rotational detachment strategies, integrated into the gait schedule for a space climbing robot. By monitoring the foot-end reaction forces in real time, the proposed method establishes adhesion without risking damaging the spacecraft exterior, and smooth detachment is achieved by rotating the foot joint instead of direct pulling. These strategies are dedicated to reducing unnecessary control actions and, accordingly, the required adhesion forces in all feet, reducing the possibility of unexpected detachment. Climbing experiments have been conducted in a suspension-based gravity compensation system to examine the merits of the proposed method. The experimental results demonstrate that the proposed rotational detaching method decreases the required pulling force by 65.5% compared to direct pulling, thus greatly reducing the disturbance introduced to the robot body and other supporting legs. When stepping on an obstacle, the compliant control method is shown to reduce unnecessarily aggressive control actions and result in a reduction in relevant normal and shear adhesion forces in the supporting legs by 44.8% and 35.1%, respectively, compared to a PID controller.

AerospaceVol. 12(1)
Shanghai Micro Satellite Engineering Center (CN), University of Chinese Academy of Sciences (CN)
Science and Technology Innovation Plan Of Shanghai Science and Technology Commission
Openalex Percentile: Top 8%
Space Satellite Systems and Control
2.60
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