Estimation Of Longitudinal Moment Derivatives Of Missile Configuration Using Semi Free Flying Technique

Rajamurthy, MS and Rajan, SR and Basappa, - and Niranjana, T (1993) Estimation Of Longitudinal Moment Derivatives Of Missile Configuration Using Semi Free Flying Technique. Technical Report. NAL, Bangalore.

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    Abstract

    A Semi-Free Dynamic Flying Test Technique Has Been Used To Estimate The Pitching Moment Derivatives Of A Missile Model. Wind Tunnel Tests Were Carried Out On A 1 :8 Scale Model Of PJ08 Missile Configuration. The Pitching Moment Derivatives Were Estimated From The Angular Motion Responses Of The Model To Doublet Input Using MLE Method. The Results Of Tests On Configuration 1 For Three CG Positions Are Detailed.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Semi-free Flying; Missile Configuration; Longitudinal Moment Derivatives
    Subjects: AERONAUTICS > Aeronautics (General)
    Division/Department: Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division
    Depositing User: M/S ICAST NAL
    Date Deposited: 25 Sep 2012 10:29
    Last Modified: 25 Sep 2012 10:29
    URI: http://nal-ir.nal.res.in/id/eprint/10983

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