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

摘要

This document is a project proposal submitted to DRDLudand details work contemplated . The work proposed consistsudof making a 1/10 scale model of a missile andudinstrumenting it for servo actuation and for rotaryudresponse sensing. By flying the model at variousudangles of attack and at various CG locations (includingudstatically 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.