CubeSat Debris Capture Using Power Rate Reaching Law Sliding Mode Control (PRRL-SMC)

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Authors: M.H. Azadmanesh, Ali Mari Oryad, Krasin Krasimirov Georgiev
Cited by: 1
References: 22

Abstract

Active Debris Removal (ADR) missions demand precise and rapid controllers that lower collision risks specifically in the capture phase of tumbling objects. Sliding Mode Control (SMC), in general, offers robustness against model uncertainties. However, traditional reaching laws often face slow convergence when the chaser is too far from the target state. In this paper, we address this particular limitation and present the first application of Power Rate Reaching Law Sliding Mode Control (PRRL-SMC) to the 6-DOF coupled dynamics of a CubeSat-based debris capture mission in both the pre-capture tracking and post-capture stabilization phases in the case of tumbling debris. To show the strength of our work, we evaluate the proposed controller against Proportional–Derivative (PD), Linear Quadratic Regulator (LQR), second-order SMC (SOSMC), and terminal SMC (TSMC) for the pre-capture tracking and post-capture stabilization phases. By numerical simulations we show that PRRL-SMC reduces convergence time extremely and achieves stable capture in 7.6 s. This time it is 24.6 s for LQR and 28.1 s for SOSMC. The controller also handles the abrupt inertia variations of the combined stack post-capture successfully. This is efficient for proximity operations because of their importance in timing and fuel conservation.

Fields of Study & Subjects

Space Satellite Systems and Control Spacecraft Dynamics and Control Astro and Planetary Science

Publication details

Journal / source
The 17th International Scientific Conference on Aerospace, Automotive, and Railway Engineering
Publisher
MDPI
Pages
25–25
Publication date
19 January 2026
Language
EN