NDLI: Monte carlo analysis of inaccuracies in estimated aircraft parameters caused by unmodeled flight instrumentation errors

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Monte carlo analysis of inaccuracies in estimated aircraft parameters caused by unmodeled flight instrumentation errors

Content Provider	NASA Technical Reports Server (NTRS)
Author	Bryant, W. H. Hodge, W. F.
Copyright Year	1975
Description	An output error estimation algorithm was used to evaluate the effects of both static and dynamic instrumentation errors on the estimation of aircraft stability and control parameters. A Monte Carlo error analysis, using simulated cruise flight data, was performed for a high-performance military aircraft, a large commercial transport, and a small general aviation aircraft. The results indicate that unmodeled instrumentation errors can cause inaccuracies in the estimated parameters which are comparable to their nominal values. However, the corresponding perturbations to the estimated output response trajectories and characteristics equation pole locations appear to be relatively small. Control input errors and dynamic lags were found to be in the most significant of the error sources evaluated.
File Size	974239
Page Count	36
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19750009296
Archival Resource Key	ark:/13960/t3nw47k5x
Language	English
Publisher Date	1975-02-01
Access Restriction	Open
Subject Keyword	Aircraft Stability And Control Aircraft Stability Error Analysis Military Aircraft Instrument Errors Flight Instruments Commercial Aircraft General Aviation Aircraft Monte Carlo Method Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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