On the Problem of Flight Dynamics
Optimization of an aircraft vertical trajectory is considered. The central idea of this study is that a complex nonlinear boundary value problem is solved using a finite number of arithmetic operations. The results of numerical simulations confirm the efficiency of this technique.
Authors
- Yu. Ya. Ostov
- A. P. Ivanov
Institutions
- St Petersburg University (RU)
Publication Details
- Journal
- Vestnik St Petersburg University Mathematics
- Published
- 2025-12-01
- DOI
- https://doi.org/10.1134/s1063454125700670
- Primary Topic
- Aerospace Engineering and Control Systems
- Type
- article
- Field-Weighted Citation Impact
- 0.00