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    Rapid Path Planning for Zero Propellant Maneuvers Based on Flatness 

    Source: Journal of Aerospace Engineering:;2017:;Volume ( 030 ):;issue: 005
    Author(s): Sheng Zhang; Qian Zhao; Hai-Bing Huang; Guo-Jin Tang
    Publisher: American Society of Civil Engineers
    Abstract: A rapid path planning (RPP) method that fast generates suboptimal zero propellant maneuver (ZPM) paths was proposed previously, and to further enhance the planning performance, the differential flatness of the model is ...
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    Analytical Prediction for Tunneling-Induced Ground Movements with Modified Deformation Pattern 

    Source: International Journal of Geomechanics:;2018:;Volume ( 018 ):;issue: 006
    Author(s): Yuan Wei;Fu HeLin;Zhang JiaBing;Huang Zhen
    Publisher: American Society of Civil Engineers
    Abstract: In current methods for predicting ground movement caused by tunneling, the center of the tunnel is usually thought of as the focus of ground-movement vectors for convenience. In reality, the ground-movement vectors around ...
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    Robust Adaptive Control for Spacecraft Rendezvous with Predefined-Time Prescribed Performance and Input Saturation 

    Source: Journal of Aerospace Engineering:;2021:;Volume ( 035 ):;issue: 001:;page 06021007
    Author(s): Yong Hao; Zhixian Lin; Ziyi Su; Yunfei Xiao; Bing Huang
    Publisher: ASCE
    Abstract: This paper proposes a robust adaptive predefined-time control scheme for spacecraft rendezvous maneuvers with the consideration of input saturation and external disturbances. To ensure the rendezvous maneuver completing ...
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    Adaptive Finite-Time Control for Attitude Tracking of Spacecraft under Input Saturation 

    Source: Journal of Aerospace Engineering:;2018:;Volume ( 031 ):;issue: 002
    Author(s): Yong Guo; Bing Huang; Shuo Wang; Ai-jun Li; Chang-qing Wang
    Publisher: American Society of Civil Engineers
    Abstract: This paper investigates two robust finite-time controllers for the attitude control of the spacecraft by using a modified terminal sliding mode surface. With the use of terminal sliding mode control and adaptive control, ...
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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