Electronics Optics & Control, Volume. 22, Issue 9, 25(2015)

Dynamic Inverse Control of Super Maneuverable Aircraft Based on Sliding Mode Observer and PI

PAN Zheng-wei... XUE Ya-li and ZHANG Hong-xiang |Show fewer author(s)
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    References(7)

    [7] [7] LEVANT A.Slidingorder and sliding accuracy in sliding mode control[J].International Journal of Control, 1993, 58(6):1247 -1263.

    [8] [8] GILBERT W P, NGUYEN L T, VAN GUNST R W.Simulator study of the effectiveness of an automatic control system designed to improve the high angle of attack charactaristics of a flighter airplane[R].Virginia:Langley Research Center, 1976.

    [9] [9] ATESOGLU?, ?ZG?REN K. High-ct flight maneuverability enhancement o£ a twin engine flight-bomber aircraft for air combat superiority using thrust-vectoring control [ C]// AIAA Guidance, Navigation, and Control Conference, Colo?rado :AIAA, 2006-6050.

    [10] [10] SNELL S A, ENNS D F, ARRARD W L.Nonlinear dynamic inversion flight control of supermaneuverable aircraft[D].Minnesota:University of Minnesota, 1991.

    [11] [11] BUGAJSKI D J, ENNS D F.Nonlinear control law with application to high angle of attack flight[J].Journal of Guidance, Control, And Dynamic, 1992, 15(3):761-767.

    [14] [14] SHTESSEL Y, TOURNES C, KRUPP D.Reusable launch vehicle control in sliding modes [C]//AIAA Guidance, Navigation, and Control Conference, New Orleans:AIAA, 1997:335-345.

    [15] [15] LEVANT A.Higher order sliding modes, differentiation and output feedback control[J].International Journal of Control, 2003, 76(9):924-941.

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    PAN Zheng-wei, XUE Ya-li, ZHANG Hong-xiang. Dynamic Inverse Control of Super Maneuverable Aircraft Based on Sliding Mode Observer and PI[J]. Electronics Optics & Control, 2015, 22(9): 25

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    Paper Information

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    Received: Nov. 17, 2014

    Accepted: --

    Published Online: Jan. 28, 2021

    The Author Email:

    DOI:10. 3969/j. issn. 1671 -637x. 2015.09.006

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