Flight Dynamics and Structural Load Distribution for a Damaged Aircraft
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-6153
Reference14 articles.
1. An Approach to Predict Flight Dynamics and Stability Derivatives of Distressed Aircraft
2. Dynamics and Adaptive Control for Stability Recovery of Damaged Asymmetric Aircraft
3. Erratum on "Flight Dynamics and Hybrid Adaptive Control of Damaged Aircraft"
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