Evaluation of Recursive Methods for Aircraft Parameter Estimation
Author:
Affiliation:
1. National Aerospace Laboratories
2. DLR Institute of Flight Systems
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-5063
Reference29 articles.
1. α Z
2. α M
3. q M
4. eMδ
5. 20 40 60 80 100 120 -6 0 20 40 60 80 100 120 1 2 3 4 5 6
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