Summary
Techniques used currently in the aeronautical industry are applied to solve several flight control law clearance tasks. The obtained results for the clearance of the HIRM+RIDE control configuration are intended to serve as basis for comparisons with several more advanced approaches presented in this book.
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References
Koehler R., Wilmes T. Revision of control law design and clearance requirements DLR-IB-111-2000/10, February 2000.
GARTEUR FM(AG11) Clearance of HIRM+RIDE nonlinear augmented aircraft model. Baseline solution. GARTEUR/TP-119-09, Oct 2000.
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© 2002 Springer-Verlag Berlin Heidelberg
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Wilmes, T. (2002). Baseline Solution. In: Fielding, C., Varga, A., Bennani, S., Selier, M. (eds) Advanced Techniques for Clearance of Flight Control Laws. Lecture Notes in Control and Information Sciences, vol 283. Springer, Berlin, Heidelberg. https://doi.org/10.1007/3-540-45864-6_15
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DOI: https://doi.org/10.1007/3-540-45864-6_15
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Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-540-44054-3
Online ISBN: 978-3-540-45864-7
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