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    Parameter Identification–Based Attitude Stabilization Control of Spacecraft with Multiaccessories during Orbital Maneuver 

    Source: Journal of Aerospace Engineering:;2017:;Volume ( 030 ):;issue: 003
    Author(s): Xiangdong Liu; Xing Xin; Zhen Li; Yongzhi Sheng; Zhen Chen
    Publisher: American Society of Civil Engineers
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    Analytic Approach and Landing Guidance through a Novel Time-Varying Sliding Mode Control Method 

    Source: Journal of Aerospace Engineering:;2016:;Volume ( 029 ):;issue: 004
    Author(s): Yao Zhao; Yongzhi Sheng; Xiangdong Liu; Zhen Li
    Publisher: American Society of Civil Engineers
    Abstract: In this paper, a nonlinear guidance law is developed for the approach and landing (A&L) phase of a reusable launch vehicle (RLV). First, a novel time-varying sliding mode control (TVSMC) technique is introduced. The main ...
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    Analytic Approach and Landing Guidance through a Novel Time-Varying Sliding Mode Control Method 

    Source: Journal of Aerospace Engineering:;2016:;Volume ( 029 ):;issue: 004
    Author(s): Yao Zhao; Yongzhi Sheng; Xiangdong Liu; Zhen Li
    Publisher: American Society of Civil Engineers
    Abstract: In this paper, a nonlinear guidance law is developed for the approach and landing (A&L) phase of a reusable launch vehicle (RLV). First, a novel time-varying sliding mode control (TVSMC) technique is introduced. The ...
    Request PDF
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     

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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