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Stability and Control characteristics of MIG-21 aircraft

Authors
Publication date
1 January 1985
Publisher
National Aerospace Laboratories

Abstract

This document provides the stability and control derivatives data for the MIG-21BIS aircraft in the form readily usable for control system synthesis. Analytical prediction of the aircraft modes, typical time responses as well as Bode plots in the frequency domain are presented. Longitudinal dynamics data presented in this document supersedes the one provided in NAL PD SE 8501

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    NAL-IR

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    Last time updated on 14/03/2018

    National Aerospace Laboratories Institutional Repository

    redirect
    oaioai:nal-ir.nal.res.in:11097
    Last time updated on 16/07/2013