Flight-test validation of a takeoff performance uncertainty model
Flight-test validation of a takeoff performance uncertainty model
A Monte Carlo model designed for fixed-wing aircraft takeoff performance uncertainty quantification is benchmarked. The uses of an efficient takeoff simulator of this type range from rapid design variable and constraint sensitivity studies and large-scale conceptual level analyses to operational performance planning and real-time anomaly detection. The accuracy of the model is assessed against high-resolution flight-test data obtained through a campaign consisting of eight takeoffs flown with a specially instrumented commuter category transport aircraft: a BAe Jetstream Series 3100 twin turboprop. On all but one of the takeoffs, a close agreement is seen in terms of the takeoff distance, as predicted vs as observed, at the point of passing a 35 ft screen height; for the outlier, evidence of a sudden change in wind speed is presented as the probable cause of the discrepancy. Such studies are subject to many other sources of error and uncertainty, which are inherent in both flight-test data analysis and simulation, stemming from the highly dynamic and complex nature of this phase of the flight. The analysis presented also proposes to be a template for dealing with these issues, in a way that is applicable to other benchmarking studies.
1216-1228
Sobester, Andras
096857b0-cad6-45ae-9ae6-e66b8cc5d81b
November 2021
Sobester, Andras
096857b0-cad6-45ae-9ae6-e66b8cc5d81b
Sobester, Andras
(2021)
Flight-test validation of a takeoff performance uncertainty model.
Journal of Aircraft, 58 (6), .
(doi:10.2514/1.C036180).
Abstract
A Monte Carlo model designed for fixed-wing aircraft takeoff performance uncertainty quantification is benchmarked. The uses of an efficient takeoff simulator of this type range from rapid design variable and constraint sensitivity studies and large-scale conceptual level analyses to operational performance planning and real-time anomaly detection. The accuracy of the model is assessed against high-resolution flight-test data obtained through a campaign consisting of eight takeoffs flown with a specially instrumented commuter category transport aircraft: a BAe Jetstream Series 3100 twin turboprop. On all but one of the takeoffs, a close agreement is seen in terms of the takeoff distance, as predicted vs as observed, at the point of passing a 35 ft screen height; for the outlier, evidence of a sudden change in wind speed is presented as the probable cause of the discrepancy. Such studies are subject to many other sources of error and uncertainty, which are inherent in both flight-test data analysis and simulation, stemming from the highly dynamic and complex nature of this phase of the flight. The analysis presented also proposes to be a template for dealing with these issues, in a way that is applicable to other benchmarking studies.
More information
Accepted/In Press date: 20 June 2021
e-pub ahead of print date: 6 August 2021
Published date: November 2021
Additional Information:
Funding Information:
The flights were funded by the School of Engineering of the University of Southampton as part of an annual educational test campaign integrated into the aeronautics and astronautics undergraduate program of the school. The development and validation of the takeoff performance model were funded by the UK Engineering and Physical Sciences Research Council under grant number EP/R009953/1 (CASCADE project). The author would like to thank Tim Takahashi, Andy Keane, and Jim Scanlan for useful discussions on uncertainty quantification, takeoff performance, and first-order performance modeling. Special thanks also go to the National Flying Laboratory Centre team from Cranfield University, who not only operated the flights, but also patiently answered the author’s questions afterward (in particular, Nick Lawson and Alastair Cooke).
Funding Information:
The flights were funded by the School of Engineering of the University of Southampton as part of an annual educational test campaign integrated into the aeronautics and astronautics undergraduate program of the school. The development and validation of the takeoff performance model were funded by the UK Engineering and Physical Sciences Research Council under grant number EP/R009953/1 (CASCADE project). The author would like to thank Tim Takahashi, Andy Keane, and Jim Scanlan for useful discussions on uncertainty quantification, takeoff performance, and first-order performance modeling. Special thanks also go to the National Flying Laboratory Centre team from Cranfield University, who not only operated the flights, but also patiently answered the author?s questions afterward (in particular, Nick Lawson and Alastair Cooke).
Publisher Copyright:
© 2021 by the authors. Published by the American Institute of Aeronautics and Astronautics, Inc.
Identifiers
Local EPrints ID: 452175
URI: http://eprints.soton.ac.uk/id/eprint/452175
ISSN: 0021-8669
PURE UUID: 9cdc266e-081c-4005-ae34-a6298000b811
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Date deposited: 29 Nov 2021 17:30
Last modified: 18 Oct 2024 01:38
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