Journal of Astronautics ›› 2019, Vol. 40 ›› Issue (6): 694-702.doi: 10.3873/j.issn.1000-1328.2019.06.010
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CHEN Jia ye, MU Rong jun, BAI Yu liang, ZHANG Xin, CUI Nai gang
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Abstract:
A sliding mode controller based on self-learning disturbance observer (SLDO) is designed for a reusable launch vehicle (RLV). According to the singular perturbation theory, a RLV dynamic model is divided into the outer-loop and inner-loop subsystems. Since the model uncertainties and the disturbances vary with time and have unknown boundaries, combining with the type-2 neuro-fuzzy structure, feedback-error learning scheme and sliding mode control (SMC) theory, a novel online SLDO is presented. The multivariable supertwisting sliding mode controller driven by a SLDO is designed to track the re-entry trajectory precisely and convergent rapidly. Finally, by the simulation and analysis of the 6-degree-of-freedom model of RLV in the reentry phase, the effectiveness and the robustness of the integrated control scheme are verified.
Key words: Reusable launch vehicle (RLV), Self-learning disturbance observer (SLDO), Sliding mode control (SMC), Reentry attitude track
CLC Number:
V249122
CHEN Jia ye, MU Rong jun, BAI Yu liang, ZHANG Xin, CUI Nai gang. Sliding Mode Control in Reentry Phase for a Reusable Launch Vehicle Driven by a Self Learning Disturbance Observer[J]. Journal of Astronautics, 2019, 40(6): 694-702.
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URL: http://www.yhxb.org.cn/EN/10.3873/j.issn.1000-1328.2019.06.010
http://www.yhxb.org.cn/EN/Y2019/V40/I6/694