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

Dition 

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

Copyright information

© Springer-Verlag London Limited 1999

Authors and Affiliations

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

Personalised recommendations