Gradient-enhanced PINN-based hybrid attitude control for reentry vehicle under uncertainties
Fields of Study & Subjects
Adaptive Dynamic Programming Control
Model Reduction and Neural Networks
Aeroelasticity and Vibration Control
Publication details
- Journal / source
- Aerospace Science and Technology
- Publisher
- Elsevier BV
- Volume
- 171
- Pages
- 111600–111600
- Publication date
- 9 January 2026
- Language
- EN