Closed-form non-iterative suboptimal control exploiting differential flatness for finite-horizon problems with application to angle-constrained guidance
Fields of Study & Subjects
Guidance and Control Systems
Spacecraft Dynamics and Control
Optimization and Variational Analysis
Publication details
- Journal / source
- Aerospace Science and Technology
- Publisher
- Elsevier BV
- Volume
- 179
- Pages
- 113298–113298
- Publication date
- 27 July 2026
- Language
- EN