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μ Method

  • Rick Lind
  • Marty Brenner
Part of the Advances in Industrial Control book series (AIC)

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.

Keywords

Stability Margin Flight Condition Flight Data Aeroelastic Model Uncertainty Operator 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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Copyright information

© Springer-Verlag London Limited 1999

Authors and Affiliations

  • Rick Lind
    • 1
  • Marty Brenner
    • 1
  1. 1.Dryden Flight Research CenterUSA

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