Flight Test Maneuvers for Efficient Aerodynamic Modeling
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031699
Reference17 articles.
1. Aircraft System Identification: Theory and Practice
2. Multiple input design for real-time parameter estimation in the frequency domain
3. Flight-Test Experiment Design for Characterizing Stability and Control of Hypersonic Vehicles
4. Real-Time Dynamic Modeling: Data Information Requirements and Flight-Test Results
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