Abstract
This chapter presents the axes, the frames, and the nonlinear model of the aircraft used in this book [1–4].
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References
B. Stevens and F. Lewis. Aircraft Control and Simulation, Second Edition. Wiley, New York, NY, 2003.
R. F. Stengel. Flight Dynamics. Princeton University Press, 2004.
M. Möckli. Guidance and Control for Aerobatic Maneuvers of an Unmanned Airplane. PhD thesis, ETH Zurich, 2006. Diss No. 16586.
G. J. J. Ducard. Fault-tolerant Flight Control and Guidance Systems for a Small Unmanned Aerial Vehicle. PhD thesis, ETH Zürich, 2007. Diss. No. 17505.
C. Eck. Navigation Algorithms with Applications to Unmanned Helicopters. PhD thesis, ETH Zürich, 2001. Diss. No. 14402.
R. Möller. Modelling an Acrobatic Aircraft. Term paper, ETH Zürich, 2003.
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© 2009 Springer London
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(2009). Nonlinear Aircraft Model. In: Fault-tolerant Flight Control and Guidance Systems. Advances in Industrial Control. Springer, London. https://doi.org/10.1007/978-1-84882-561-1_3
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DOI: https://doi.org/10.1007/978-1-84882-561-1_3
Publisher Name: Springer, London
Print ISBN: 978-1-84882-560-4
Online ISBN: 978-1-84882-561-1
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