A nonlinear integral-uncertainty observer is presented, which can estimate the integral of measurement output signal and the uncertainty in system, synchronously. In order to be satisfied with the existing hardware computational environments and to select the parameters more easily, a simplified linear version of the nonlinear integral-uncertainty observer is also developed. The effectiveness of the proposed observers is verified through the numerical simulations and experiments: First, through the integral-uncertainty observers, the attitude angle and the uncertainties in attitude dynamics are estimated synchronously from the measurements of angular velocity, and the estimate results by the two observers are compared; second, a control law is designed based on the observers to drive the jet aircraft to track a reference trajectory.


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    Title :

    Navigation and Control Based on Integral-Uncertainty Observer for Unmanned Jet Aircraft


    Contributors:
    Xinhua Wang, (author) / Lilong Cai, (author)


    Publication date :

    2017-06-01


    Size :

    5029813 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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