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    Robust Control of PVTOL Aircraft with a Nonlinear Optimal Control Solution 

    Source: Journal of Aerospace Engineering:;2010:;Volume ( 023 ):;issue: 004
    Author(s): Ming Xin; Hejia Pan
    Publisher: American Society of Civil Engineers
    Abstract: In this paper, a new nonlinear control strategy is proposed for hovering control of planar vertical takeoff and landing (PVTOL) aircraft. The control of this typical nonlinear, nonminimum-phase system is treated as a robust ...
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    Trajectory Control of Miniature Helicopters Using a Unified Nonlinear Optimal Control Technique 

    Source: Journal of Dynamic Systems, Measurement, and Control:;2011:;volume( 133 ):;issue: 006:;page 61001
    Author(s): Ming Xin; Yunjun Xu; Ricky Hopkins
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: It is always a challenge to design a real-time optimal full flight envelope controller for a miniature helicopter due to the nonlinear, underactuated, uncertain, and highly coupled nature of ...
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    Position and Attitude Control of Deep-Space Spacecraft Formation Flying Via Virtual Structure and θ-D Technique 

    Source: Journal of Dynamic Systems, Measurement, and Control:;2007:;volume( 129 ):;issue: 005:;page 689
    Author(s): Ming Xin; S. N. Balakrishnan; H. J. Pernicka
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Control of deep-space spacecraft formation flying is investigated in this paper using the virtual structure approach and the θ-D suboptimal control technique. The circular restricted three-body ...
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian