Since high-speed unmanned drones do not need landing gear design, they usually take off with zero-length launch methods such as rocket-assisted or catapult launch. In this paper, for a certain type of unmanned target drone, by analyzing the zero-length take-off process and force changes of the unmanned target drone, a dynamic model of the unmanned target drone rocket-assisted zero-length launch process is established. Considering the unmanned target drone with the servo system, engine system, booster rocket and other models of the drone and the dynamic state change model of the drone during take-off, a set of take-off control laws for a certain type of drone rocket to boost the zero-length launch was designed. Simulink simulation tool has carried out the simulation verification of the take-off process, and verified the feasibility of the take-off and the rationality of the control law design of this unmanned target drone under the design conditions.


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    Title :

    UAV Zero-Length Launch Control Law Design


    Additional title:

    Lect. Notes Electrical Eng.


    Contributors:
    Yan, Liang (editor) / Duan, Haibin (editor) / Deng, Yimin (editor) / He, Chengchan (author) / Sun, Zonghua (author) / Wu, Liaoni (author)

    Conference:

    International Conference on Guidance, Navigation and Control ; 2022 ; Harbin, China August 05, 2022 - August 07, 2022



    Publication date :

    2023-01-31


    Size :

    9 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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