Stability and Control characteristics of MIG-21 aircraft

Bhagawan, BS and Parameswaran, V and Rajeswari, Ramamurthy S and Sridhar, JK and Srinatha Sastry, CV and Ramabhadran, S and Seshadri, SN and Sundaramurthy, H and Yegna Narayan, K (1985) Stability and Control characteristics of MIG-21 aircraft. Project Report. National Aerospace Laboratories, Bangalore.

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    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.

    Item Type: Proj.Doc/Technical Report (Project Report)
    Uncontrolled Keywords: Stability derivatives;Control derivatives;Eigen values; Transfer function;Aircraft mathematical models;Aircraft modes/responses
    Subjects: ENGINEERING > Engineering (General)
    Division/Department: Systems Engineering Division, Systems Engineering Division, C-CADD, Systems Engineering Division, Systems Engineering Division, Aerodynamics, Aerodynamics, Aerodynamics, Experimental Aerodynamics Division
    Depositing User: Smt Bhagya Rekha KA
    Date Deposited: 27 Nov 2012 14:11
    Last Modified: 13 Oct 2015 13:42
    URI: http://nal-ir.nal.res.in/id/eprint/11100

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