The dynamic characteristics of aerospace vehicles (ASVs) and the design of control systems significantly impact closed-loop performance. This study presents an integrated system design approach based on the ASV-integrated control-oriented model. By incorporating control-related open-loop constraints and optimizing fuel consumption during the dynamic pressure acceleration climb segment, the research conducts an integrated design of airframe/trajectory. Performance constraints linked to the control system are integrated into the optimization problem of the body/thrust system, and the simulation results indicate the need for comprehensive consideration of subsystem constraints and performance.


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    Title :

    Integrated Design of the Airframe and Trajectory of Aerospace Vehicles


    Additional title:

    Lect. Notes Electrical Eng.


    Contributors:
    Yan, Liang (editor) / Duan, Haibin (editor) / Deng, Yimin (editor) / Sun, Zhijun (author) / Liu, Biao (author) / Li, Yibo (author) / Xu, Liang (author)

    Conference:

    International Conference on Guidance, Navigation and Control ; 2024 ; Changsha, China August 09, 2024 - August 11, 2024



    Publication date :

    2025-03-04


    Size :

    11 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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    R. J. Matt / J. B. Muratore / R. E. Murteza et al. | NTIS | 1963


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