• Electronics Optics & Control
  • Vol. 28, Issue 5, 23 (2021)
CHEN Yuan1, ZHOU Li1、2, LIU Zhenkai1, YAO Bo1, and LING Zhihao1
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
  • show less
    DOI: 10.3969/j.issn.1671-637x.2021.05.006 Cite this Article
    CHEN Yuan, ZHOU Li, LIU Zhenkai, YAO Bo, LING Zhihao. A Robust Predictive Sliding Mode Attitude Control Method for Hypersonic Vehicles[J]. Electronics Optics & Control, 2021, 28(5): 23 Copy Citation Text show less
    References

    [10] GUO J G, ZHANG T B, CHENG C,et al.Model reference adaptive attitude control for near space hypersonic vehicle with mismatched uncertainties [J].Transactions of the Institute of Measurement and Control, 2019, 41(5):1301-1312.

    [12] FIDAN B, MIRMIRANI M,IOANNOU P A.Flight dynamics and control of air-breathing hypersonic vehicles:review and new directions[C]//The 12th AIAA International Space Planes and Hypersonic Systems and Te-chnologies, 2003:1-24.

    [18] TANG K, WANG W, MENG Y, et al.Flight control and airwake suppression algorithm for carrier landing based on model predictive control [J].Transactions of the Institute of Measurement and Control, 2019, 41(8):2205-2213.

    CHEN Yuan, ZHOU Li, LIU Zhenkai, YAO Bo, LING Zhihao. A Robust Predictive Sliding Mode Attitude Control Method for Hypersonic Vehicles[J]. Electronics Optics & Control, 2021, 28(5): 23
    Download Citation