Moment Stability Derivatives of Prithvi Missile Configuration at Low Speed Using Semi Free Dynamic Flying Method -Proposal

Balakrishna, S and Niranjana, T (1986) Moment Stability Derivatives of Prithvi Missile Configuration at Low Speed Using Semi Free Dynamic Flying Method -Proposal. Project Report. National Aerospace Laboratories, Bangalore.

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    Abstract

    This document is a project proposal submitted to DRDL and details work contemplated . The work proposed consists of making a 1/10 scale model of a missile and instrumenting it for servo actuation and for rotary response sensing. By flying the model at various angles of attack and at various CG locations (including statically unstable case with a control law invoked.) The responses to a known control surface input is analysed using MLE technique and the moment derivatives and trim are generated. This data is relevant in design of missile control design and specifically at low speeds when the missile will be statically unstable.

    Item Type: Proj.Doc/Technical Report (Project Report)
    Uncontrolled Keywords: Semi free flying, Moment stability derivatives, Missile
    Subjects: AERONAUTICS > Aircraft Stability and Control
    Division/Department: Systems Engineering Division, Systems Engineering Division
    Depositing User: Smt Bhagya Rekha KA
    Date Deposited: 03 May 2012 16:28
    Last Modified: 03 May 2012 16:28
    URI: http://nal-ir.nal.res.in/id/eprint/10444

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