Flight Control Law Design using Hybrid Incremental Nonlinear Dynamic Inversion
Author:
Affiliation:
1. Roketsan Roket Sanayii ve Ticaret AS
2. Technische Universiteit Delft Faculteit Luchtvaart- en Ruimtevaarttechniek
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-1597
Reference34 articles.
1. An integrated approach to flight control design using dynamic inversion and μ-synthesis
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4. A simplified approach to nonlinear dynamic inversion based flight control
5. Flight test experience of a non-linear dynamic inversion control law on the VAAC Harrier
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