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.

Format:

Book

Author/Creator:

Cannarsa, Piermarco.

Contributor:

Celletti, Alessandra.

Fasano, Giorgio.

Mazzini, Leonardo.

Pontani, Mauro.

Trélat, Emmanuel.

Series:

Springer Optimization and Its Applications, 1931-6836 ; 221

Language:

English

Subjects (All):

Mathematical optimization.

System theory.

Control theory.

Aerospace engineering.

Astronautics.

Optimization.

Systems Theory, Control.

Aerospace Technology and Astronautics.

Local Subjects:

Optimization.

Systems Theory, Control.

Aerospace Technology and Astronautics.

Physical Description:

1 online resource (312 pages)

Edition:

1st ed. 2025.

Place of Publication:

Cham : Springer Nature Switzerland : Imprint: Springer, 2025.

Summary:

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 an overview of the most important current topics concerning optimal control in space. Optimal control theory is an exciting research area, where both new theoretical approaches and application problems come into play. The “New Trends and Challenges in Optimization Theory Applied to Space Engineering” conference brought together influential academic researchers and experts from industry and government to build bridges between their respective groups. The topics of the conference panels are selected to include the most advanced areas of interest for space applications. In line with the mission of the Gran Sasso Tech Foundation, interdisciplinary dialogue is promoted between the sciences, and different experts are encouraged to work together to identify new problems and generate new solutions. Covering a wide range of space-related topics and challenges, this conference aims to lay the foundation for a long-term collaboration between different groups of experts. A broad overview of control theory applications in space is presented, highlighting the most recent aspects, both from a theoretical and practical point of view, in particular on the following topics: - manifold dynamics, trajectory design and related control aspects; - AI techniques in guidance control problems and space missions; - optimization techniques for constellations with applications to space operations; - multi-stage control problems for launch and landing problems; - optimal control problems in the presence of uncertain parameters; - improved sufficient and necessary conditions in optimal control problems for space problems. New methods, specific mathematical models, ad hoc algorithms and heuristics, innovative mission scenarios, and advances in classical control theory are presented.

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.

Notes:

Description based on publisher supplied metadata and other sources.

ISBN:

9783031812538

OCLC:

1530375030