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Fast Terminal Sliding Mode Control for the Soft Landing of a Space Robot on an Asteroid Considering a Barycentric Gravitational Model

عنوان مقاله: Fast Terminal Sliding Mode Control for the Soft Landing of a Space Robot on an Asteroid Considering a Barycentric Gravitational Model
شناسه ملی مقاله: AEROSPACE21_045
منتشر شده در بیست و یکمین کنفرانس بین المللی انجمن هوا فضای ایران در سال 1401
مشخصات نویسندگان مقاله:

Mahsa Azadmanesh - K.N.Toosi University of Technology, Tehran, Iran.
Jafar Roshanian - K.N.Toosi University of Technology, Tehran, Iran.
Mostafa Hassanalian - New Mexico Tech University, Socorro, New Mexico, US.

خلاصه مقاله:
This study aims to control a space robot's soft-landing trajectory on the asteroid EROS۴۳۳ considering a weak, yet effective gravitational field. As the research innovation, the study employs a fast terminal sliding mode control (FTSMC) to manage the landing trajectory and enhance the dynamic tracking performance for the soft landing of the space robot on the asteroid. This controller can ensure that the system modes are positioned on the sliding surface within a limited time. As an advantage over the PD sliding mode controller, the proposed controller raises the speed and improves the accuracy of tracking the desired trajectory and enhances the robustness of the control system. The study further compares the results of simulations performed in MATLAB to evaluate the proposed controller design.

کلمات کلیدی:
Space Robot Landing, Fast Terminal Sliding Mode Control, Asteroid, Lyapunov Stability.

صفحه اختصاصی مقاله و دریافت فایل کامل: https://civilica.com/doc/1668288/