Abstract
In order to reduce development costs and time, model-based design is widely introduced in the industry leading to a strong need for verified high-fidelity simulation models. An inevitable, but challenging process step to obtain such simulation models for GNC-applications is the aerodynamic parameter identification on the basis of real flight test data. The identification process requires distinct excitation maneuvers in order to constrain the design space to a subset of model parameters reducing the complexity of the identification problem and the correlation within the overall parameter set. Typically, manually flown excitation maneuvers are not exact and fully reproducible concerning the requirements and therefore the amount of rejected data points is significant. In case of remotely piloted aircraft systems, the decoupling of the aircraft and the ground pilot in charge leads to an even less sensitive maneuver control, a further reduced disturbance suppression and even greater difficulties in meeting the initialization requirements. This scenario calls for an automation of aerodynamic parameter identification related flight tests. A practical approach to a flight test oriented autopilot for improved aerodynamic parameter identification is proposed within this paper. The requirements for identification excitation maneuvers and the corresponding design of the autopilot are emphasized and flight test results are presented.
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References
Krings, M., Thielecke, F.: An Integrated Approach to Predictive Flight Guidance and Envelope Protection. In: AIAA Guidance, Navigation and Control Conference, AIAA–2012–4712, AIAA (Augest 2012)
Krings, M., Thielecke, F.: Ein Integrierter Ansatz für ein Prädiktives Autopiloten- und Flugbereichssicherungssystem. In: Deutscher Luft- und Raumfahrtkongress, DGLR (September 2012)
Henrichfreise, H., Bensch, L., et al.: Estimation of Gusts and Structural Loads for Commercial Aircraft. In: International Forum on Aeroelasticity and Structural Dynamics. CEAS/AIAA (June 2009)
Haar, J., Montel, M., et al.: Flight Test Aircraft SPRINT for Loads Observer Assesment. In: International Workshop on Aircraft System Technologies. Shaker Verlag (April 2011)
Montel, M., Haar, J., Thielecke, F.: Modellierung und Identifikation der Längsbewegung des Flugversuchsträgers UW-9 SPRINT zur Modellbasierten Beobachtung von Strukturlasten. In: Deutscher Luft- und Raumfahrtkongress, DGLR (September 2011)
Montel, M., Haar, J., Thielecke, F.: Identifikation der Seitenbewegung und Validierung des Aerodynamischen Gesamtmodells für den Flugversuchsträger UW-9 SPRINT. In: Deutscher Luft- und Raumfahrtkongress, DGLR (September 2012)
Jategaonkar, R.V.: Flight Vehicle System Identification: A Time Domain Methodology. AIAA, Reston (2006)
Klein, V., Morelli, E.A.: Aircraft System Identification: Theory and Practice. AIAA, Reston (2006)
Brockhaus, R., Alles, W., Luckner, R.: Flugregelung. Springer-Verlag GmbH, Heidelberg (2011)
Mulder, J.A.: Design and Evaluation of Dynamic Flight Test Manoeuvres. Deflt University of Technology, Delft (1986)
Mulder, J.A., Sridhar, J.K., Breeman, J.H.: Identification of Dynamic Systems - Applications to Aircraft. AGARD Flight Test Techniques Series, Part 2, NATO Advisory Group for Aerospace Research and Development (1994)
Morelli, E.A.: Flight Test Validation of Optimal Input Design and Comparison to Conventional Inputs. In: AIAA Atmospheric Flight Mechanics Conference. AIAA (1997)
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Krings, M., Henning, K., Thielecke, F. (2013). Flight Test Oriented Autopilot Design for Improved Aerodynamic Parameter Identification. In: Chu, Q., Mulder, B., Choukroun, D., van Kampen, EJ., de Visser, C., Looye, G. (eds) Advances in Aerospace Guidance, Navigation and Control. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-38253-6_17
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DOI: https://doi.org/10.1007/978-3-642-38253-6_17
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-38252-9
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