Adaptive Smooth Control via Nonsingular Fast Terminal Sliding Mode for Distributed Space Telescope Demonstration Mission by CubeSat Formation Flying

التفاصيل البيبلوغرافية
العنوان: Adaptive Smooth Control via Nonsingular Fast Terminal Sliding Mode for Distributed Space Telescope Demonstration Mission by CubeSat Formation Flying
المؤلفون: Jeon, Soobin, Cho, Hancheol, Park, Sang-Young
سنة النشر: 2024
المجموعة: Computer Science
مصطلحات موضوعية: Electrical Engineering and Systems Science - Systems and Control
الوصف: This paper investigates the efficiency of nonsingular fast terminal sliding mode and adaptive smooth control method for the distributed space telescope demonstration mission. The distributed space telescope has a flexible focal length that corresponds to the relative position of the formation flying concept. The precise formation flying technology by CubeSats enhances the utility of distributed space systems with low costs. The propulsion systems for CubeSats usually have restricted degrees of freedom. Since the scientific mission requires continuous orbit control, the attitude and orbit control system mutually affect the control performance. The nonsingular fast terminal sliding mode has the advantage of a fast convergence rate and is able to improve the control performance. The adaptive smooth controller designed for the SISO system is expanded and applied to the attitude and orbit control system. The simulation results verify the efficiency of the adaptive smooth controller based on the nonsingular fast terminal sliding mode.
Comment: This manuscript is submitted to IEEE Transactions on Aerospace and Electronic Systems
نوع الوثيقة: Working Paper
URL الوصول: http://arxiv.org/abs/2402.04718
رقم الأكسشن: edsarx.2402.04718
قاعدة البيانات: arXiv