A New Formulation of the Filter-Error Method for Aerodynamic Parameter Estimation in Turbulence
Author:
Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-2704
Reference28 articles.
1. Aircraft System Identification: Theory and Practice
2. 2Maine, R. and Iliff, K. “Identification of Dynamic Systems: Theory and Formulation,” Tech. Rep. RP-1138, NASA, Edwards, CA, February 1985.
3. Application of System Identification to Aircraft at NASA Langley Research Center
4. Retrospective and Recent Examples of Aircraft Parameter Identification at NASA Dryden Flight Research Center
5. Practical Aspects of the Equation-Error Method for Aircraft Parameter Estimation
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