Control Design for Soft Transition for Landing Preparation of Light Compound-Wing Unmanned Aerial Vehicles Based on Incremental Nonlinear Dynamic Inversion.
- Resource Type
- Article
- Source
- Applied Sciences (2076-3417); Nov2023, Vol. 13 Issue 22, p12225, 21p
- Subject
ANGULAR acceleration LANDING (Aeronautics) ELECTRIC switchgear PHYSICAL constants PHASE transitions ACCELERATION (Mechanics) - Language
- ISSN
- 20763417