Collision response and obstacle avoidance of the tethered-space net robot system with non-target objects

Abstract

Purpose

This paper aims to study the encounter issues of the Tethered-Space Net Robot System (TSNRS) with non-target objects on orbit during the maneuver, including the collision issues with small space debris and the obstacle avoidance from large obstacles.

Design/methodology/approach

For the collision of TSNRS with small debris, the available collision model of the tethered net and its limitation is discussed, and the collision detection method is improved. Then the dynamic response of TSNRS is studied and a closed-loop controller is designed. For the obstacle avoidance, the variable enveloping circle of the TSNRS has coupled with the artificial potential field (APF) method. In addition, the APF is improved with a local trajectory correction method to avoid the overbending segment of the trajectory.

Findings

The collision model coupled with the improved collision detection method solves the detection failure and speeds up calculation efficiency by 12 times. Collisions of TSNRS with small debris make the local thread stretch and deforms finally making the net a mess. The boundary of the disturbance is obtained by a series of collision tests, and the designed controller not only achieved the tracking control of the TSNRS but also suppressed the disturbance of the net.

Practical implications

This paper fills the gap in the research on the collision of the tethered net with small debris and makes the collision model more general and efficient by improving the collision detection method. And the coupled obstacle avoidance method makes the process of obstacle avoidance safer and smoother.

Originality/value

The work in this paper provides a reference for the on-orbit application of TSNRS in the active space debris removal mission.

Citation

Zhu, W., Pang, Z., Si, J. and Du, Z. (2022), "Collision response and obstacle avoidance of the tethered-space net robot system with non-target objects", Aircraft Engineering and Aerospace Technology, Vol. 94 No. 5, pp. 715-733. https://doi.org/10.1108/AEAT-07-2021-0208