Maximum Likelihood Identification of Aircraft Stability and Control Derivatives
Author:
Affiliation:
1. Harvard University, Cambridge, Mass.
2. Systems Control, Inc., Palo Alto, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.60327
Reference11 articles.
1. Identification of stochastic linear dynamic systems using Kalman filter representation
2. Identification in automatic control systems
3. Comparison of some methods used for process identification
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