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: Monograph (Project Report)
Uncontrolled Keywords: Semi free flying, Moment stability derivatives, Missile
Subjects: AERONAUTICS > Aircraft Stability and Control
Depositing User: Smt Bhagya Rekha KA
Date Deposited: 03 May 2012 10:58
Last Modified: 03 May 2012 10:58
URI: http://nal-ir.nal.res.in/id/eprint/10444

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