Electronics Optics & Control, Volume. 28, Issue 8, 77(2021)

Dynamics Boundary Protection for Aircraft Landing Based on Reachable Set

QIU Xiaonan1... ZHANG Jiuxing2, LI Yinghui1, LI Xiaohua1 and DONG Zehong1 |Show fewer author(s)
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    References(13)

    [1] [1] Statistical summary of commercial jet airplane accidentsworldwide operations1959-2015[EB/OL].(2016-07-01)[2020-09-04].http://www.boeing.com/news/techissues/pdf/statsum.pdf.

    [6] [6] BRAGG M BHUTCHISON TMERRET Jet al.Effect of ice accretion on aircraft flight dynamics:AIAA-2000-0360[C/OL].(2000-01-10)[2020-09-04].https://doi.org/10.2514/6.2000-360.

    [7] [7] RANAUDO R JMARTOS BNORTON B Wet al.Piloted simulation to evaluate the utility of a real time envelope protection system for mitigating in-flight icing hazards:AIAA-2010-7987[R/OL].(2011-10-01)[2020-09-04].http://www.sti.nasa.gov.

    [8] [8] DICKEY E DPRINCEN N HBONET J Tet al.Wind tunnel model design and fabrication of a 5.75% scale blended-wing-body twin jet configuration:AIAA-2016-0008[C/OL].(2016-01-04)[2020-09-04].https://doi.org/10.2514/6.2016-0008.

    [9] [9] BALACHANDRAN SATKINS E M.Flight safety assessment and management to prevent loss of control due to in-flight icing:AIAA-2016-0094[C/OL].(2016-01-04)[2020-09-04].https://doi.org/10.2514/6.2016-0094.

    [10] [10] VERESNIKOV G SEGOROV N AKULIDA E Let al.Methods for solving of the aircraft landing problem.I.exact solution methods[J].Automation and Remote Control201980:1317-1334.

    [11] [11] DONG Z HLI Y HZHENG W Jet al.Optimization control for aircraft based on manifold theory[J].Journal of Aircraft201855(6):2549-2553.

    [14] [14] LOMBAERTS T J JSCHUET S RWHEELER K Ret al.Safe maneuvering envelope estimation based on a physical approach[C]//AIAA GuidanceNavigationand Control (GNC) Conference2013:1-20.

    [15] [15] GINGRAS D RBARNHART BRANAUDO Ret al.Envelope protection for in-flight ice contamination:NASA/TM—2010-216072[C/OL].(2009-01-05)[2020-09-04].https://doi.org/10.2514/6.2009-1458.

    [17] [17] JORDAN TLANGFORD WBELCASTRO Cet al.Development of a dynamically scaled generic transport model testbed for flight research experiments[R].WashingtonD.C.:NASA2004.

    [18] [18] KWATNY H GDONGMO J TCHANG B Cet al.Nonlinear analysis of aircraft loss of control[J].Journal of GuidanceControland Dynamics201336(1):149-162.

    [19] [19] LYGEROS J.On reachability and minimum cost optimal control[J].Automatica200440(6):917-927.

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    QIU Xiaonan, ZHANG Jiuxing, LI Yinghui, LI Xiaohua, DONG Zehong. Dynamics Boundary Protection for Aircraft Landing Based on Reachable Set[J]. Electronics Optics & Control, 2021, 28(8): 77

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    Paper Information

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    Received: Sep. 4, 2020

    Accepted: --

    Published Online: Aug. 16, 2021

    The Author Email:

    DOI:10.3969/j.issn.1671-637x.2021.08.016

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