Abstract
Generating a model by analyzing flight data is essential for computing a confident stability analysis. A nominal model generated purely from analytical equations of the predicted aircraft dynamics may not accurately describe the true aircraft; therefore, a model must be generated that accounts for the flight data to ensure the predicted dynamics represent the true dynamics.
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© 1999 Springer-Verlag London Limited
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Lind, R., Brenner, M. (1999). μ Method. In: Robust Aeroservoelastic Stability Analysis. Advances in Industrial Control. Springer, London. https://doi.org/10.1007/978-1-4471-0849-8_9
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DOI: https://doi.org/10.1007/978-1-4471-0849-8_9
Publisher Name: Springer, London
Print ISBN: 978-1-4471-1215-0
Online ISBN: 978-1-4471-0849-8
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