The problem of guiding an instrumented aircraft to follow a preassigned trajectory using the Portable Automatic Calibration Tracker (PACT) data is considered in this paper. Guidance control is formulated as an optimal linear state regulator problem for a discrete time-delayed system. Responses to some flight courses of interest have been achieved through computer system simulation. Post-flight test data obtained from the PACT confirm the basic validity of the theoretical results.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Automatic flight guidance using the portable automatic calibration tracker data


    Additional title:

    Automatische Fluganleitung durch den Einsatz portabler automatisch kalibrierter Gleichlauf-Daten


    Contributors:

    Published in:

    Publication date :

    1975


    Size :

    , 7 Quellen



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English






    Flight data tracker

    ZUBAIRI JUNAID AHMED | European Patent Office | 2017

    Free access

    Flight Data Tracker

    ZUBAIRI JUNAID AHMED | European Patent Office | 2015

    Free access