• Electronics Optics & Control
  • Vol. 31, Issue 11, 109 (2024)
WU Yunyan, HUANG Tianpeng, LIU Wu, ZHU Xueyao, and MA Zhao
Author Affiliations
  • Xi'an Flight Automatic Control Research Institute, AVIC, Xi'an 710000, China
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    DOI: 10.3969/j.issn.1671-637x.2024.11.016 Cite this Article
    WU Yunyan, HUANG Tianpeng, LIU Wu, ZHU Xueyao, MA Zhao. Adaptive Unscented Kalman Filter Based Estimation of Aircraft Airflow Angles[J]. Electronics Optics & Control, 2024, 31(11): 109 Copy Citation Text show less
    References

    [1] ANGELINI R, DENARO A. IXV re-entry demonstrator: mission overview, system challenges and flight reward[J]. Acta Astronautica, 2016, 124: 18-30.

    [2] WANG Q, WU K Y, ZHANG T J, et al. Aerodynamic modeling and parameter estimation from QAR data of an airplane approaching a high-altitude airport[J]. Chinese Journal of Aeronautics, 2012, 25(3): 361-371.

    [3] WISE K. Flight testing of the X-45A J-UCAS computational alpha-beta system[C]//AIAA Guidance, Navigation, and Control Conference and Exhibit. Keystone: AIAA, 2006: 21-24.

    [5] HE Q Z, ZHANG W G, LIU X X, et al. Information fusion and reconstruction of key sensors in a flight control system in constant wind field based on two stage EKF[C]//2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC). Nanjing: IEEE, 2017: 718-724.

    WU Yunyan, HUANG Tianpeng, LIU Wu, ZHU Xueyao, MA Zhao. Adaptive Unscented Kalman Filter Based Estimation of Aircraft Airflow Angles[J]. Electronics Optics & Control, 2024, 31(11): 109
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