This paper considers a given set of fixed order compensators for aircraft pitch control problem. By augmenting compensator variables to the original state equations of the aircraft, a new dynamic model is considered to seek a LQ controller. While the fixed order compensators can achieve a set of desired poles in a specified region, LQ formulation provides the inherent robustness properties. The time response for ride quality is significantly improved with a set of dynamic compensators.


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    Title :

    Aircraft Pitch Control with Fixed Order LQ Compensators


    Contributors:


    Publication date :

    1997-02-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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