This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Status of Dynamic Flight Test Technology -Model Identification for Flight Simulation
Annotation ability available
Sector:
Language:
English
Abstract
Dynamic flight test technology has by now emerged as a valuable tool for assessment of aircraft performance characteristics and stability and control characteristics. In this paper emphasis is on applications In the context of flight simulation. It is shown that after flight path reconstruction and reconstruction of the motion of the primary control system a linear and stepwise identification procedure can be applied for the development of aerodynamic models and models of primary control force characteristics. These models can be implemented in mathematical models for aircraft flight simulation.
Topic
Citation
Mulder, J. and den Hollander, J., "Status of Dynamic Flight Test Technology -Model Identification for Flight Simulation," SAE Technical Paper 810597, 1981, https://doi.org/10.4271/810597.Also In
References
- Binkhorst H. van der Snoek L. non-published measurements on a 1:11 scale model of the DeHavilland DHC-2 “Beaver” laboratory aircraft in symmetrical and asymmetrical flow conditions in the low speed windtunnel of Delft University of Technology, Department of Aerospace Engineering 1977
- Deutsch R. “Estimation Theory” Prentice Hall, Englewood Cliffs, N.J 1965
- Etkin B. “Dynamics of AtmosphericFlight” John Wiley and Sons, Inc New York 1972
- Garretson H.C. III “Beaver aircraft parameter identification - technical preparations and preliminary results” Deutsche For-schungs- and Versuchsanstalt for Luft- and Raumfahrt, DFVLR-Mitt. 78-01 1978
- Gerlach O.H. “The determination of stability derivatives and performance characteristics from dynamics maneuvers” AGARD Conference Proceedings No. 85 1971 Delft University of Technology, Department of Aerospace Engineering 1971
- den Hollander J.G. “Identification of primary flight control system characteristics from dynamic flight tests” To be published as a Report of Delft University of Technology, Department of Aerospace Engineering
- Hall W.E. Grysta N.K. Tyler J.S. “Model structure determination and parameter identification for nonlinear aerodynamic flight regimes” AGARD Conference Proceedings No. 172 on “Methods for aircraft state and parameter identification”, Hampton, Virginia November 1974
- Hosman R.J.A.W. van der Vaart J.C. “Thresholds of motion perception and parameters of vestibular models obtained from tests in a motion simulator. Effects of vestibular and visual motion perception on task performance” Memorandum M-372, Delft University of Technology, Department of Aerospace Engineering Delft, The Netherlands August 1980 August 24-29 1980
- Iliff K.W. Maine R.E. “Practical aspects of using a maximum likelihood estimation method to extract stability and control derivatives from flight data” 1976
- Iliff K.W. “Aircraft identification experience”. AGARD Lecture Series No. 104 on: “Parameter Identification” Delft, London October 29-30 November 1-2 1979
- Key D.L. “Fidelity of simulation for pilot training.”
- Klein V. Schiess J.R. “Compatibility check of measured aircraft response using kinematic equations and extended Kalmanfilter” 1977
- Mulder J.A. “Estimation of the aircraft state In non-steady flight” AGARD Conference Proceedings No. 172 on “Methods for Aircraft state and parameter identification”, Hampton, Virginia November 1974
- Mulder J.A. van Sliedregt J.M. “Estimation of drag and thrust of jet-propelled aircraft by non-steady flight test manoeuvres” AGARD Conference Proceedings No. 223 on “Flight Test Techniques”, Porz Wahn, Germany, October 1976
- Mulder J.A. Jonkers H.L. Horsten J.J. Breeman J.H. Simons J.L. “Analysis of aircraft performance, stability and control measurements” AGARD Lecture Series No. 104 on: “Parameter Identification” Delft London, October 29-30 November 1-2 1979
- Plaetschke E. Schultz G. “Practical input design” AGARD LectureSeries No. 104 on: Parameter Identification, Delft, Londen October 29-30 November 1-2 1979
- Stalford H.L. “Application of the estimation - before - modelling (EBM) system identification method to the high angle of attack/side slip flight of the T-2c jet trainer aircraft” Dynamics Research Corporation, System Division 60 Concord Street, Wilmington November 1979
- Viersma T.J. Baarspul M. “Development and application of a moving-base visual flight simulator, including the design of hydraulic actuators with hydrostatic bearings” Memorandum M-371, Delft University of Technology, Department of Aerospace Engineering, Delft, The Netherlands, June, 1980 (paper presented at the 12th Congress of the International Council of the Aeronautical Sciences, Munich October 12-17 1980
- Wingrove R.C. “Applications of a technique for estimating aircraft states from recorded flight test data” AIAA paper No.72-965 September 1972