Real-Time Parameter Estimation using Output Error-Reference-Cited by-同舟云学术

Real-Time Parameter Estimation using Output Error

Published:2014-06-13 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference
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Author:

Grauer Jared A.¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2014-2556

Reference26 articles.

1. 1Taylor, L. and Iliff, K. “System Identification Using a Modified Newton-Raphson Method - A FORTRAN Program,” Tech. Rep. TN-D-6734, NASA, Washington, D.C., May 1972.

2. 2Maine, R. and Iliff, K. “A FORTRAN Program for Determining Aircraft Stability and Control Derivatives From Flight Data,” Tech. Rep. TN-D-7831, NASA, Edwards, CA, April 1975.

3. 3Maine, R. and Iliff, K. “User’s Manual for MMLE3, a General FORTRAN Program for Maximum Likelihood Parameter Estimation,” Tech. Rep. Technical Paper 1563, NASA, Edwards, CA, November 1980.

4. 4Murray, J. and Maine, R. “pEst Version 2.1 User’s Manual,” Tech. Rep. TM-88280, NASA, Edwards, CA, September 1987.

5. Aircraft System Identification: Theory and Practice

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