Sliding mode control and observation techniques are widely used in aerospace applications, including aircraft, UAVs, launch vehicles (LVs), missile interceptors, and hypersonic missiles. This work is dedicated to creating an MATLAB-based sliding mode controller design and simulation software toolbox that aims to support aerospace vehicle applications. An architecture of the aerospace sliding mode control toolbox (SMC Aero) using the relative degree approach is proposed. The SMC Aero libraries include first-order sliding mode control, second-order sliding mode control, and higher order sliding mode control (either fixed gain or adaptive), as well as higher order sliding mode differentiators. The efficacy of the SMC Aero toolbox is confirmed in two case studies: 1) controlling and 2) simulating resource prospector lander soft landing on the Moon and LV attitude control in ascent mode.


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    Title :

    Development of Relative Degree-Based Aerospace Sliding Mode Control MATLAB Toolbox With Case Studies


    Contributors:


    Publication date :

    2024-09-01


    Size :

    2125268 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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