The Flight Management System (FMS) on civil aircraft takes responsibility for flight planning, position calculation, performance calculation, and flight guidance. Performance Database (PDB) stores necessary aircraft-specific performance data to allow FMS to carry out the related functions. To solve the PDB compliance issue, the first-principal design method in the PDB development process is introduced to allow more accurate trajectory prediction in complex flight scenarios. In this method, PDB includes full engine performance data, performance limits, and aerodynamic data. To ensure the database quality and integrity, the methods of combining the element-level testing and system-level functional verification are investigated to demonstrate the onboard PDB satisfies the system function, performance, and airworthiness requirements based on engineer practice.


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    Title :

    Study on Design and Verification Method of Civil Aircraft Onboard Flight Management System Performance Database


    Additional title:

    Lect. Notes Electrical Eng.


    Contributors:
    Yan, Liang (editor) / Duan, Haibin (editor) / Deng, Yimin (editor) / Liu, Lizhao (author)

    Conference:

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



    Publication date :

    2025-02-28


    Size :

    10 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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