Buch, Englisch, Band 200, 399 Seiten, Format (B × H): 160 mm x 241 mm, Gewicht: 787 g
New Concepts and Approaches
Buch, Englisch, Band 200, 399 Seiten, Format (B × H): 160 mm x 241 mm, Gewicht: 787 g
Reihe: Springer Optimization and Its Applications
ISBN: 978-3-031-24811-5
Verlag: Springer International Publishing
Zielgruppe
Research
Autoren/Hrsg.
Fachgebiete
- Technische Wissenschaften Verkehrstechnik | Transportgewerbe Luft- und Raumfahrttechnik, Luftverkehr
- Mathematik | Informatik EDV | Informatik Informatik Künstliche Intelligenz
- Mathematik | Informatik Mathematik Numerik und Wissenschaftliches Rechnen Optimierung
- Mathematik | Informatik Mathematik Geometrie Dynamische Systeme
- Technische Wissenschaften Maschinenbau | Werkstoffkunde Technische Mechanik | Werkstoffkunde Statik, Dynamik, Kinetik, Kinematik
- Mathematik | Informatik Mathematik Operations Research
Weitere Infos & Material
Advances in the Control Propellant Minimization for the Next Generation Gravity Mission (A. Anselmi ).- Transition of Two-dimensional Quasi-periodic Invariant Tori in the Real-ephemeris Model of the Earth-Moon System (N. Baresi).- Hypersonic Point-to-Point Travel for the Common Man (E. Mooij).- Bifocal Metrology Applications in Space Engineering (F. Bresciani).- A Revisited Analysis of the Radioisotope Sail and its Possible Application to Relativistic Spaceflight (L. Derosa).- The ERC-Funded EXTREMA Project: Achieving Self-Driving Interplanetary CubeSats (G. Di Domenico).- Data Reduction for Optimizing the Attitude Control Dispatch in a Spacecraft (C. Durand).- Second Order Suf?cient Conditions of Strong Minimality with applications to Orbital Transfers (L. Mazzini).- Evolutionary Optimisation of a Flexible-Launcher Simple Adaptive Control System (E. Mooij).- Optimization and Solution Approaches in Utilizing Wireless Sensor Networks for Exploring Moon Planets and Space (O. Ozkan).- Near-Optimal Guidance and Pulse-Modulated Reduced Attitude Control for Orbit Injection (M. Pontani).- A Pareto front numerical reconstruction strategy applied to a satellite system conceptual design (M. Sebastián).- Indirect optimization of robust orbit transfer considering thruster underperformance (F. Simeoni).- Time-Varying Lyapunov Control Laws with Enhanced Estimation of Distribution Algorithm for Low-Thrust Trajectory Design (R. Armellin).