• Electronics Optics & Control
  • Vol. 23, Issue 11, 33 (2016)
FU Peng, ZHOU Xin, and YUAN Suo-zhong
Author Affiliations
  • [in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2016.11.008 Cite this Article
    FU Peng, ZHOU Xin, YUAN Suo-zhong. NDI-PID Based Control Law Design for Aircraft Approaching in Low-Altitude Windshear[J]. Electronics Optics & Control, 2016, 23(11): 33 Copy Citation Text show less
    References

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    [7] HINTON D A.Flight-management strategies for escape from microburst encounters, tm 4057[R].Washington, DC: National Aeronautics and Space Administration Press, 1988.

    [8] SACHS G, GRIGAT E.Optimal 3-dimensional trajectories for microburst escape [C]//AIAA the 22nd Atmospheric Flight Mechanics Conference, 1997: 814-821.

    [14] Department of Transportation Federal Aviation Administration.TSO-C117a airborne windshear warning and escape guidance system for transport airplane[S].Washington, DC: FAA Aircraft Certification Service, 1990: 47-51.

    FU Peng, ZHOU Xin, YUAN Suo-zhong. NDI-PID Based Control Law Design for Aircraft Approaching in Low-Altitude Windshear[J]. Electronics Optics & Control, 2016, 23(11): 33
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