It is challenging to control a UAV during the actuator failure because it is a highly nonlinear, coupled, underactuated system. Partial UAV control is achievable by reallocating the control signals, but control over one state has to be compromised, which would be the yaw angle for the quadrotor UAVs.


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    Title :

    Deflecting Surface-Based Total Rotor Failure Compensation for Biplane Quadrotor


    Additional title:

    Studies in Systems, Decision and Control


    Contributors:


    Publication date :

    2023-02-24


    Size :

    19 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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