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| Link zu diesem Datensatz | https://d-nb.info/1380770130 |
| Titel | New Trends and Challenges in Optimization Theory Applied to Space Engineering : OTSE Conference Proceedings, 13‒15 December 2023, L'Aquila (Italy) / edited by Piermarco Cannarsa, Alessandra Celletti, Giorgio Fasano, Leonardo Mazzini, Mauro Pontani, Emmanuel Trélat |
| Person(en) |
Cannarsa, Piermarco (Herausgeber) Celletti, Alessandra (Herausgeber) Fasano, Giorgio (Herausgeber) Mazzini, Leonardo (Herausgeber) Pontani, Mauro (Herausgeber) Trélat, Emmanuel (Herausgeber) |
| Organisation(en) | SpringerLink (Online service) (Sonstige) |
| Ausgabe | 1st ed. 2025 |
| Verlag | Cham : Springer Nature Switzerland, Imprint: Springer |
| Zeitliche Einordnung | Erscheinungsdatum: 2025 |
| Umfang/Format | Online-Ressource, XIV, 221 p. 67 illus., 61 illus. in color. : online resource. |
| Andere Ausgabe(n) |
Printed edition:: ISBN: 978-3-031-81252-1 Printed edition:: ISBN: 978-3-031-81254-5 Printed edition:: ISBN: 978-3-031-81255-2 |
| Inhalt | Intoduction -- Manifold dynamics, trajectory design, and control aspects -- Pontryagin’s Principle for the Optimization of Escape Trajectories from Earth-Moon L2 -- AI techniques in guidance control problem and space missions -- On Emerging Guidance Control Problems in the Satellite Industry -- Artificial Intelligence Algorithm for Space Missions -- Optimization techniques for constellations with applications in space operations -- An Integer Linear Programming Model for Earth Observation Missions -- In-orbit Servicing and Assisted Orbit Transfer Mission Planning -- Multi-stage control for launcher and landing problems -- Preliminary End-to-End Lunar Mission Design using Direct Optimization Method -- Optimal control for the moon lander: the classical problem and variants -- Optimal control problems in the presence of uncertain parameters -- Robust Minimum-fuel orbit transfers taking into account thruster under-performance -- Improved sufficient and necessary conditions in optimal control problems for aerospace problems -- Optimal Feedback Control of Astrodynamic Systems Using Solutions of the Hamilton-Jacobi-Bellman Equation -- Second-order sufficient conditions for weak local minima: general control constraints -- Multi-arc Spacecraft Trajectory Optimization |
| Persistent Identifier |
URN: urn:nbn:de:101:1-2511050307286.376441058557 DOI: 10.1007/978-3-031-81253-8 |
| URL | https://doi.org/10.1007/978-3-031-81253-8 |
| ISBN/Einband/Preis | 978-3-031-81253-8 |
| Sprache(n) | Englisch (eng) |
| Beziehungen | Springer Optimization and Its Applications ; 221 |
| DDC-Notation | 006.3 (maschinell ermittelte DDC-Kurznotation) |
| Sachgruppe(n) | 004 Informatik |
| Online-Zugriff | Archivobjekt öffnen |
Treffer 5 von 491
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