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New Trends and Challenges in Optimization Theory Applied to Space Engineering OTSE Conference Proceedings, 13‒15 December 2023, L'Aquila (Italy) /

The book consists of the proceedings of the workshop "New Trends and Challenges in Optimization Theory Applied to Space Engineering", held in l'Aquila (Italy), and organized by the Gran Sasso Science Institute (GSSI), on December 13-15, 2023. The main purpose of the book is to provide...

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Detalles Bibliográficos
Autor Corporativo: SpringerLink (Online service)
Outros autores: Cannarsa, Piermarco (Editor), Celletti, Alessandra (Editor), Fasano, Giorgio (Editor), Mazzini, Leonardo (Editor), Pontani, Mauro (Editor), Trélat, Emmanuel (Editor)
Formato: Electrónico eBook
Idioma:inglés
Publicado: Cham : Springer Nature Switzerland : Imprint: Springer, 2025.
Edición:1st ed. 2025.
Series:Springer Optimization and Its Applications, 221
Subjects:
Mathematical optimization.
System theory.
Control theory.
Aerospace engineering.
Astronautics.
Optimization.
Systems Theory, Control.
Aerospace Technology and Astronautics.
Acceso en liña:https://doi.org/10.1007/978-3-031-81253-8
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Table of Contents:
  • 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.

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