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Parameter estimation techniques and application in aircraft flight testingTechnical papers presented at the symposium by selected representatives from industry, universities, and various Air Force, Navy, and NASA installations are given. The topics covered include the newest developments in identification techniques, the most recent flight-test experience, and the projected potential for the near future.
Document ID
19740017456
Acquisition Source
Legacy CDMS
Document Type
Book
Date Acquired
September 3, 2013
Publication Date
April 1, 1974
Subject Category
Aircraft
Report/Patent Number
H-806
NASA-TN-D-7647
Report Number: H-806
Report Number: NASA-TN-D-7647
Accession Number
74N25569
Funding Number(s)
PROJECT: RTOP 501-26-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19740017457WorkAn overview of parameter estimation techniques and applications in aircraft flight testing19740017458WorkA survey of AFFDL parameter estimation efforts and future plans19740017459WorkNavy participation in the development of airframe parameter identification techniques19740017460WorkA comparison of two methods of extracting stability derivatives from flight test data19740017461WorkExtraction of derivatives from flight data for several aircraft, using the LRC interactive computer system19740017462WorkIdentification of aircraft stability and control derivatives in the presence of turbulence19740017463WorkIdentification of M2/F3 stability and control derivatives from flight data containing gust effects19740017464WorkEstimation of longitudinal aerodynamic coefficients and comparison with wind-tunnel values19740017465WorkApplication of a Kalman filter identification technique to flight data from the X-22A variable stability V/STOL aircraft19740017466WorkHelicopter derivative identification from analytic models and flight test data19740017467WorkNonlinear parameter identification: Ballistic range experience applicable to flight testing19740017468WorkIdentification of aircraft stability and control parameters using multilevel, hierarchical estimation19740017469WorkParameter estimation using an a posteriori criterion19740017470WorkA square root formulation for the combined state-parameter estimator with application to the identification of sailplane performance19740017471WorkA unified approach to aircraft parameter identification19740017472WorkEffects of flight instrumentation errors on the estimation of aircraft stability and control derivatives19740017473WorkParameter identifiability of linear dynamical systems19740017474WorkA new criterion for modeling systems19740017475WorkA practical scheme for adaptive aircraft flight control systems19740017476WorkEstimation of elastic aircraft parameters using the maximum likelihood method19740017477WorkEstimation of structural parameters from dynamic test data19740017478WorkDetermination of propulsion-system-induced forces and moments of a Mach 3 cruise aircraft19740017479WorkSystems identification - reprise and projections19740017480WorkSome after-dinner reflections on system identification19740017457WorkAn overview of parameter estimation techniques and applications in aircraft flight testing19740017458WorkA survey of AFFDL parameter estimation efforts and future plans19740017459WorkNavy participation in the development of airframe parameter identification techniques19740017460WorkA comparison of two methods of extracting stability derivatives from flight test data19740017461WorkExtraction of derivatives from flight data for several aircraft, using the LRC interactive computer system19740017462WorkIdentification of aircraft stability and control derivatives in the presence of turbulence19740017463WorkIdentification of M2/F3 stability and control derivatives from flight data containing gust effects19740017464WorkEstimation of longitudinal aerodynamic coefficients and comparison with wind-tunnel values19740017465WorkApplication of a Kalman filter identification technique to flight data from the X-22A variable stability V/STOL aircraft19740017466WorkHelicopter derivative identification from analytic models and flight test data19740017467WorkNonlinear parameter identification: Ballistic range experience applicable to flight testing19740017468WorkIdentification of aircraft stability and control parameters using multilevel, hierarchical estimation19740017469WorkParameter estimation using an a posteriori criterion19740017470WorkA square root formulation for the combined state-parameter estimator with application to the identification of sailplane performance19740017471WorkA unified approach to aircraft parameter identification19740017472WorkEffects of flight instrumentation errors on the estimation of aircraft stability and control derivatives19740017473WorkParameter identifiability of linear dynamical systems19740017474WorkA new criterion for modeling systems19740017475WorkA practical scheme for adaptive aircraft flight control systems19740017476WorkEstimation of elastic aircraft parameters using the maximum likelihood method19740017477WorkEstimation of structural parameters from dynamic test data19740017478WorkDetermination of propulsion-system-induced forces and moments of a Mach 3 cruise aircraft19740017479WorkSystems identification - reprise and projections19740017480WorkSome after-dinner reflections on system identification
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