Stability result for dynamic inversion devised to control large flexible aircraft
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-4284
Reference9 articles.
1. Dynamic inversion: an evolving methodology for flight control design
2. Dynamic inversion to control large flexible transport aircraft
3. Stability of dynamic inversion control laws applied to nonlinear aircraft pitch-axis models
4. La Salle, J.P.The Stability of Dynamical Systems.RegionalConferenceSeries in Applied Mathematics,vol.25, 1976.
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