Linear Models For The - LCA 645-33

Padma, Madhuranath and Rekha, R and Srinathkumar, S (1991) Linear Models For The - LCA 645-33. Technical Report. NAL, Bangalore.

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    The Stability Analysis And Control Law Design Of The Contemplated Light Combat Aircraft Needs Derivation Of Linear Aircraft Models From Non-Linear Flight Simulation Models . This Document Presents The Linear Longitudinal And Lateral State And Observation Models-Of The LCA Version 645-33 Obtained From NAL Developed Software For A Dozen Representative Conditions In The Flight Envelope . Poles And Zeros Of The Corresponding - Transfer Functions Have Been Generated And Compared With Those. Obtained By The Aircraft Prime.The Comparisons Give Confidence In The Use Of The Models Obtained From The NAL . Software For Control Law Design.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Linear Models; Combat Aircraft; -Flight Simulation; Control Law Design Aid
    Subjects: ASTRONAUTICS > Astronautics (General)
    Division/Department: Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division
    Depositing User: M/S ICAST NAL
    Date Deposited: 24 Aug 2012 10:05
    Last Modified: 24 Aug 2015 15:20

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