Change search
ReferencesLink to record
Permanent link

Direct link
Estimation of Aerodynamic Parameters in Real-Time: Implementation and Comparison of a Sequential Frequency Domain Method and a Batch Method
Linköping University, Department of Management and Engineering, Fluid and Mechatronic Systems.
2016 (English)Independent thesis Advanced level (degree of Master (Two Years)), 20 credits / 30 HE creditsStudent thesis
Abstract [en]

The flight testing and evaluation of collected data must be efficient during intensive flight-test programs such as the ones conducted during development of new aircraft. The aim of this thesis has thus been to produce a first version of an aerodynamic derivative estimation program that is to be used during real-time flight tests. The program is to give a first estimate of the aerodynamic derivatives as well as check the quality of the data collected and thus serve as a decision support during tests.

The work that has been performed includes processing of data in order to use it in computations, comparing a batch and a sequential estimation method using real-time data and programming a user interface. All computations and programming has been done in Matlab.

The estimation methods that have been compared are both built on transforming data to the frequency domain using a Chirp z-transform and then estimating the aerodynamic derivatives using complex least squares with instrumental variables.The sequential frequency domain method performs estimates at a given interval while the batch method performs one estimation at the end of the maneuver. Both methods compared in this thesis produce equal results. The continuous updates of the sequential method was however found to be better suited for a real-time application than the single estimation of the batch method.

The telemetric data received from the aircraft must be synchronized to a common frequency of 60 Hz. Missing samples of the data stream must be linearly interpolated and different units of measured parameters must be corrected in order to be able to perform these estimations in the real-time test environment.

Place, publisher, year, edition, pages
2016. , 62 p.
Keyword [en]
Aerodynamic coefficients, least squares, chirp z-transform, instrumental variables, missing data
National Category
Aerospace Engineering
URN: urn:nbn:se:liu:diva-132807ISRN: LIU-IEI-TEK-A–16/02498–SEOAI: diva2:1050382
External cooperation
Saab AB
Subject / course
Fluid and Mechanical Engineering Systems
Available from: 2016-11-29 Created: 2016-11-28 Last updated: 2016-11-29Bibliographically approved

Open Access in DiVA

fulltext(993 kB)13 downloads
File information
File name FULLTEXT01.pdfFile size 993 kBChecksum SHA-512
Type fulltextMimetype application/pdf

Search in DiVA

By author/editor
Nyman, Lina
By organisation
Fluid and Mechatronic Systems
Aerospace Engineering

Search outside of DiVA

GoogleGoogle Scholar
Total: 13 downloads
The number of downloads is the sum of all downloads of full texts. It may include eg previous versions that are now no longer available

Total: 20 hits
ReferencesLink to record
Permanent link

Direct link