| Citation: | YANG Zhenshu, MAO Qi, DOU Liqianet al. Interval type-2 adaptive fuzzy sliding mode control design of reentry attitude for reusable launch vehicles[J]. Journal of Beijing University of Aeronautics and Astronautics, 2020, 46(4): 781-790. doi: 10.13700/j.bh.1001-5965.2019.0474(in Chinese)
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Considering the attitude tracking problem for reusable launch vehicles (RLVs) during reentry phase with high nonlinear and multi-variable coupling characteristics in the presence of parameter uncertainties and external disturbances, an interval type-2 adaptive fuzzy sliding mode based attitude control method is proposed in this paper. Firstly, the dynamic model for the RLV is developed, which is further transformed into attitude angle and angular rate subsystems using backstepping method. Secondly, the parameter uncertainties and external disturbances of the RLV model are regarded as part of the nonlinear terms of the subsystems. Thirdly, the nonlinear terms of the subsystems are approximated by the interval type-2 fuzzy system, while the virtual control signal and the actual control signal can be obtained respectively by combining the adaptive technique and sliding mode control method. Besides, the first-order low-pass filter is used to deal with the virtual control law of subsystem. The stability of the closed-loop control system is guaranteed via Lyapunov theory and the attitude tracking error can converge to a small neighborhood around the origin. Finally, the numerical simulation on the reentry vehicle is conducted to verify that the developed control method can track the reference commands effectively and have strong robustness again external disturbances.
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