An analytic investigation has been made of procedures for effecting recovery from equilibrium spin conditions for three assumed aircraft configurations. Three approaches which utilize conventional aerodynamic controls are investigated. Included are a constant control recovery mode, optimal recoveries, and a suboptimal control logic patterned after optimal recovery results. The optimal and suboptimal techniques are shown to yield a significant improvement in recovery performance over that attained by using a constant control recovery procedure. (Author)


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    Title :

    Optimal and Suboptimal Control Technique for Aircraft Spin Recovery


    Contributors:
    J. W. Young (author)

    Publication date :

    1974


    Size :

    29 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






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