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    Aircraft Closed-Loop Dynamic System Identification in the Entire Flight Envelope Range Based on Deep Learning 

    Source: Journal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 006:;page 04024079-1
    Author(s): Zhigang Wang; Aijun Li; Yi Mi; Hongshi Lu; Changqing Wang
    Publisher: American Society of Civil Engineers
    Abstract: To solve the aircraft dynamics modeling problem in the entire envelope range, this work proposes a closed-loop system identification method based on deep learning. A closed-loop flight test was designed, under the framework ...
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    Deployment of Tethered Satellites in Low-Eccentricity Orbits Using Adaptive Sliding Mode Control 

    Source: Journal of Aerospace Engineering:;2017:;Volume ( 030 ):;issue: 006
    Author(s): Changqing Wang; Panbing Wang; Aijun Li; Yong Guo
    Publisher: American Society of Civil Engineers
    Abstract: Tethered-satellite systems have great potential in completing various space missions. However, existing researches mainly focus on the deployment of satellites in a circular orbit, whereas deployment in an elliptical orbit, ...
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    Characterizations and Optimization for Resilient Manufacturing Systems With Considerations of Process Uncertainties 

    Source: Journal of Computing and Information Science in Engineering:;2022:;volume( 023 ):;issue: 001:;page 11007
    Author(s): Ma, Qiyang;Che, Yiming;Cheng, Changqing;Wang, Zimo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The recent COVID19 pandemic reveals the vulnerability of global supply chains: the unforeseen supply crunches and unpredictable variability in customer demands lead to catastrophic disruption to production planning and ...
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    Spin-Up and Appointed Time Attitude Control of Tethered Spacecraft for Artificial Gravity 

    Source: Journal of Aerospace Engineering:;2023:;Volume ( 036 ):;issue: 005:;page 04023054-1
    Author(s): Haochang Tian; Aijun Li; Changqing Wang; Yu Wang; Yanfang Li
    Publisher: ASCE
    Abstract: This paper investigates an artificial gravity strategy using the spinning tethered spacecraft (STS), which is spun along orbital direction. An appointed-time prescribed performance (ATPP) attitude controller of tethered ...
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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