Disturbance observer-based nonfragile fuzzy tracking control of a spacecraft. Issue 9 (1st May 2023)

• Record Type: Journal Article
• Authors: Han, Tae Joon; Kim, Han Sol
• Is Part Of: Advances in space research. Volume 71:Issue 9(2023)
• Page Start: 3600
• Page End: 3612
• Publication Date: 2023-05-01
• Subjects: Spacecraft -- Tracking control -- Takagi–Sugeno (T–S) fuzzy model -- Disturbance observer-based (DOB) control -- Nonfragile control; T-S Takagi-Sugeno -- LMI Linear matrix inequality -- DOB Disturbance observer -- MRP Modified Rodrigues parameter; Space sciences -- Periodicals; Astronautics -- Periodicals; Geophysics -- Periodicals; 500.505
• DOI: 10.1016/j.asr.2022.11.043
• Languages: English
• ISSNs: 0273-1177

Abstract

Abstract: This paper deals with the nonfragile fuzzy tracking control technique of a spacecraft subject to external disturbances and control gain uncertainties. First, the Takagi–Sugeno (T–S) fuzzy model of the tracking error dynamics is newly derived. Unlike the existing studies, we assume that the controller output is norm bounded and its gain matrix is perturbed because of the aging of the actuator. Next, a fuzzy disturbance observer (DOB) estimating the external disturbance is constructed to enhance the robustness of the control system. Then, a fuzzy controller feeding back the estimated disturbance is designed to attenuate external disturbances. In addition, we establish the linear matrix inequality (LMI) conditions, by which both the H ∞ disturbance attenuating performance and the asymptotic stabilization are guaranteed. From the solution to the LMI conditions, we obtain the controller and DOB gain matrices. Finally, a simulation example validates the disturbance estimation and tracking performance of the proposed method.