This document deals with an algorithm for generating Ideal Handling Quality Models for the Longitudinal Axes of modern high performance aircraft when a flight condition is specified. The technique solves a set of non-linear equations which express the performance requirements in terms of the unknown equivalent aircraft stability and control derivatives of the ideal models. The software package is developed using PC-MATLAB and the ideal HQ models are analyzed using the HQ package already developed. The designer can directly incorporate the ideal HQ models as reference models for his feedback synthesis.


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    Title :

    Ideal Aircraft Handling Quality Models: Longitudinal Axis


    Contributors:
    S. Ismail (author) / S. Chetty (author)

    Publication date :

    1992


    Size :

    18 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English