Formation Control of Spacecraft Based on <italic>SE</italic>(3) With Asymmetric Saturated Input
In this paper, a set of integrated control problems for distributed spacecraft formation with input asymmetric constraints under external disturbances are studied. First, a new configuration error function is designed based on the compact nonlinear manifold <inline-formula> <tex-math notati...
| Main Authors: | , , , , |
|---|---|
| Formato: | Artigo |
| Idioma: | English |
| Publicado em: |
IEEE
2023-01-01
|
| Colecção: | IEEE Access |
| Assuntos: | |
| Acesso em linha: | https://ieeexplore.ieee.org/document/10322723/ |