Adaptive Nonlinear Flight Control of STOL-Aircraft Based on Incremental Nonlinear Dynamic Inversion
Author:
Affiliation:
1. Technical University of Braunschweig
2. German Aerospace Center (DLR)
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-3257
Reference37 articles.
1. SFB 880: fundamentals of high lift for future commercial aircraft
2. Multidisciplinary conceptual design for aircraft with circulation control high-lift systems
3. Flight Mechanical Challenges of STOL Aircraft Using Active High-Lift
4. Numerical investigations of aerodynamic properties of a propeller blown circulation control system on a high wing aircraft
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