Development of Closed-Loop Tail-Sizing Criteria for a High Speed Civil Transport
Author:
Affiliation:
1. Naval Postgraduate School, Monterey, California 93943
2. 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/10.2514/2.2226
Reference14 articles.
1. Limitations of statically unstable aircraft due to the effects of sensor noise, turbulence, and structural dynamics
2. On the integrated control of flexible supersonic transport aircraft
3. Integrated aircraft-controller design using linear matrix inequalities
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