Design and Analysis of a Launcher Flight Control System Based on Incremental Nonlinear Dynamic Inversion
This paper investigates the application of Incremental Nonlinear Dynamic Inversion (INDI) for launch vehicle flight control, addressing the limited exploration of nonlinear control architectures and their potential benefits in the context of the current “New Space” era. In this context, this study a...
Enregistré dans:
| Auteurs principaux: | , , |
|---|---|
| Format: | Artigo |
| Langue: | Inglês |
| Publié: |
MDPI AG
2025-03-01
|
| Collection: | Aerospace |
| Sujets: | |
| Accès en ligne: | https://www.mdpi.com/2226-4310/12/4/296 |
| Tags: |
Pas de tags, Soyez le premier à ajouter un tag!
|