Engine Yaw Augmentation for Hybrid-Wing-Body Aircraft via Optimal Control Allocation Techniques
Author:
Affiliation:
1. NASA Dryden Flight Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-6253
Reference18 articles.
1. Flight testing a propulsion-controlled aircraft emergency flight control system on an F-15 airplane
2. Flight-Test Results of Propulsion-Only Emergency Control System on MD-11 Airplane
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1. Method for Improving the Natural Lateral-Directional Stability of Flying Wings;Journal of Aerospace Engineering;2016-09
2. Dihedral influence on lateral–directional dynamic stability on large aspect ratio tailless flying wing aircraft;Chinese Journal of Aeronautics;2014-10
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