• Electronics Optics & Control
  • Vol. 21, Issue 11, 14 (2014)
GONG Qing-kun1、2, JIANG Chang-sheng1, WU Qing-xian1, and CHEN Mou1
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2014.11.003 Cite this Article
    GONG Qing-kun, JIANG Chang-sheng, WU Qing-xian, CHEN Mou. SMDO Based Super-Maneuverable Flight Control for Fighters[J]. Electronics Optics & Control, 2014, 21(11): 14 Copy Citation Text show less

    Abstract

    Considering the uncertain factors as modeling errors and external disturbances existed in nonlinear systems,a Nonlinear Dynamic Inversion (NDI) control method was proposed based on Sliding Mode Disturbance Observer (SMDO) on-line compensation.The SMDO was designed for estimating the uncertain factors,and the output of it was used to design a new compensating control law,which was used together with NDI control for eliminating the influence of the uncertain factors.The simulation experiment based on Herbst maneuver is given to show the difference between the simplex NDI control and the proposed method.The simulation results show the effectiveness and robustness of the proposed method.
    GONG Qing-kun, JIANG Chang-sheng, WU Qing-xian, CHEN Mou. SMDO Based Super-Maneuverable Flight Control for Fighters[J]. Electronics Optics & Control, 2014, 21(11): 14
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