Flight Test Specification for Missile Parameter Identification

Mohan Ram, VS and Raol, JR and Jagadeesh, M (1987) Flight Test Specification for Missile Parameter Identification. Project Report. National Aerospace Laboratories, Bangalore.

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    Abstract

    This document describes a -method of selecting and specifying a suitable test input signal for aerodynamic parameter identification of a missile with the autopilot in the loop, Recommendations for implementation of a parameter identification flight test program in the altitude range of 18 km to 5 km using a chain of doublet input signals are proposed in this document

    Item Type: Proj.Doc/Technical Report (Project Report)
    Uncontrolled Keywords: Flight Test specification, Missile Parameter Identification
    Subjects: AERONAUTICS > Aircraft Stability and Control
    Division/Department: Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division
    Depositing User: Ms Indrani V
    Date Deposited: 06 Jul 2012 16:10
    Last Modified: 25 Jun 2013 13:35
    URI: http://nal-ir.nal.res.in/id/eprint/10525

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