LMI-based robust incremental nonlinear dynamic inversion centralized design for flight attitude control
Fields of Study & Subjects
Adaptive Control of Nonlinear Systems
Aerospace and Aviation Technology
Stability and Control of Uncertain Systems
Publication details
- Journal / source
- Aerospace Science and Technology
- Publisher
- Elsevier BV
- Volume
- 172
- Pages
- 111656–111656
- Publication date
- 11 January 2026
- Language
- EN