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This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License
Identification of Continuous-Time Linear Aircraft Models Using Subspace Identification
Atsushi Fujimori
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DOI:10.17265/2332-8258/2016.01.002
This paper considers the possibility of estimating continuous-time linear aircraft models by using the subspace identification. The outline of the subspace identification for estimating the continuous-time linear model is first mentioned. The identification simulation in which the subspace identification is then applied to the modeling of aircraft in the lateral motion is performed. As a result, the continuous-time linear aircraft model is appropriately estimated by the subspace identification if the amount of the measurement noise is not so much.
Subspace identification, aircraft model, aerodynamic derivatives.
[1] Verhaegen, M., and Verdult, V. 2007. Filtering and System Identification—A Least Square Approach. Cambridge University Press.
[2] Overschee, P., and Moor, B. 1996. Subspace Identification for Linear Systems. Kluwer Academic Publishers.
[3] Schmit, L. V. 1998. Introduction to Aircraft Dynamics. AIAA.
[4] Feuer, A., and Goodwin, G. C. 1996. Sampling in Digital Signal Processing and Control. Birkhauser.
[5] Vinnicombe, G. 2001. Uncertainty and Feedback (H_inf Loop-Shaping and the V-Gap Metric). Imperial College Press.
[6] Isozaki, K., Masuda, K., Taniuchi, A., and Watari, M. 1980. “Flight Test Evaluation of Variable Stability Airplane.” KHI. Tech. Rev. 75: 50-8.