Jategaonkar, RV (1986) Flight test plan/instrumentation system for MIG-21 aircraft parameter estimation. Project Report. National Aerospace Laboratories, Bangalore.
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Abstract
Various aspects of flight instrumentation system, comprising of aircraft motion sensors, data acquisition, signal conditioning unit and magnetic tape recorder, to be used for on-board flight test data acquisition have been discussed. Appropriate flight test programme has been worked out for MIG-21 aircraft to enable estimation of both longitudinal and lateral stability and control derivatives. A brief discussion about different types of control inputs suitable for parameter estimation has also been presented.
Item Type: | Monograph (Project Report) |
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Uncontrolled Keywords: | Parameter estimation, Maximum likelihood, Flight test, On-board instrumentation |
Subjects: | AERONAUTICS > Avionics & Aircraft Instrumentation |
Depositing User: | Smt Bhagya Rekha KA |
Date Deposited: | 11 Apr 2012 11:03 |
Last Modified: | 11 Apr 2012 11:03 |
URI: | http://nal-ir.nal.res.in/id/eprint/10428 |
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