DO 28D1 aircraft parameter identification

Rajamurthy, MS (1985) DO 28D1 aircraft parameter identification. Technical Report. National Aeronautical Laboratory, Bangalore, India.

[img] PDF
tm_se_8501_p._48.pdf
Restricted to Repository staff only

Download (770kB)

Abstract

Analysis of flight test data obtained for the identification of DO 28D1 research aircraft of TU Braunschweig is detailed in this report. The data analysis was done to understand aspects related to the aircraft parameter identification from flight test data, particularly in the context of this aircraft's instrumentation and data acquisition and for planning future flight tests for obtaining flight data for13; identification purposes.

Item Type: Monograph (Technical Report)
Uncontrolled Keywords: Aircraft parameter estimation;Maximum likelihood method;Flight data analysis;Measurement errors
Subjects: AERONAUTICS > Aeronautics (General)
Depositing User: Users 90 not found.
Date Deposited: 27 Nov 2006
Last Modified: 24 May 2010 04:23
URI: http://nal-ir.nal.res.in/id/eprint/3521

Actions (login required)

View Item View Item