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High-reliability autonomous management systems for spacecraft /

"This book examines the autonomous management of spacecraft, which uses modern control technologies such as artificial intelligence to establish a remote intelligent body on the spacecraft so that the spacecraft can complete its flight tasks by itself. Its goal is to accurately perceive its own...

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Dades bibliogràfiques
Autors principals: Zhang, Jianjun (Writer on artificial satellites) (Autor), Li, Jing (Autor)
Format: Electrònic eBook
Idioma:anglès
Publicat: Amsterdam, Netherlands ; Cambridge, MA, United States : Elsevier, [2023]
Matèries:
Space vehicles > Command control systems > Management.
Véhicules spatiaux > Systèmes de commande > Gestion.
Accés en línia:ScienceDirect
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Taula de continguts:
  • Front Cover
  • High-Reliability Autonomous Management Systems for Spacecraft
  • Copyright Page
  • Contents
  • Preface
  • I. Introduction
  • 1 Spacecraft self-service management connotation
  • 1.1 Autonomous capability of spacecraft
  • 1.2 The concept of spacecraft autonomous management
  • 1.2.1 The concept of spacecraft autonomous management
  • 1.2.2 The level of spacecraft autonomous management
  • 1.2.3 Advantages of spacecraft autonomous management
  • 1.3 Aspects of autonomous management spacecraft
  • 1.3.1 Autonomous health management
  • 1.3.2 Autonomous task management
  • 1.3.3 Autonomous data management
  • 1.4 Core functions of autonomous management of spacecraft
  • 1.4.1 The model of spacecraft autonomous management
  • 1.4.2 composition of spacecraft autonomous management system
  • 1.4.2.1 Independent management
  • 1.4.2.2 Design principles of spacecraft autonomous management system
  • 1.4.2.3 Composition and function of spacecraft autonomous management system
  • References
  • 2 Spacecraft systems
  • 2.1 Spacecraft concept
  • 2.1.1 Classification of spacecraft
  • 2.1.1.1 Communication satellites
  • 2.1.1.2 Navigation satellites
  • 2.1.1.3 Remote sensing satellites
  • 2.1.1.4 Scientific exploration and technology test satellite
  • 2.1.1.5 Deep space probe
  • 2.1.1.6 Manned spacecraft
  • 2.1.2 Composition of spacecraft
  • 2.2 Basic principles of spacecraft flight
  • 2.2.1 The first cosmic velocity
  • 2.2.2 The second cosmic velocity
  • 2.2.3 The third cosmic velocity
  • 2.3 Aerospace engineering systems
  • 2.4 Preliminary idea of the plan
  • 2.4.1 Preliminary selection of spacecraft mission orbits
  • 2.4.2 Preliminary assumption of payload
  • 2.4.3 Preliminary assumption of platform subsystem
  • 2.4.3.1 Control subsystem scheme requirements and types
  • 2.4.3.1.1 Requirements for the control subsystem
  • 2.4.3.1.2 Attitude stabilization scheme
  • 2.4.3.2 Requirements and types of propulsion subsystem scheme
  • 2.4.3.2.1 Requirements for propulsion subsystem
  • 2.4.3.2.2 The type of propulsion system
  • 2.4.3.3 Types and requirements of power subsystem schemes
  • 2.4.3.3.1 Spacecraft power system requirements
  • 2.4.3.3.2 Type of spacecraft power supply
  • 2.4.3.4 Program requirements and types of measurement, control and data management subsystem
  • 2.4.3.4.1 Type of subsystem scheme
  • 2.4.3.4.2 Requirements for subsystem
  • 2.4.3.5 Type and requirements of thermal control subsystem scheme
  • 2.4.3.5.1 Requirements for thermal control subsystem
  • 2.4.3.5.2 Common methods of the thermal control subsystem
  • References
  • II. Spacecraft autonomous health management
  • 3 Spacecraft autonomous health management connotation
  • 3.1 The connotation of spacecraft health management
  • 3.1.1 Spacecraft fault
  • 3.1.2 The connotation of spacecraft management
  • 3.1.3 Understanding of spacecraft health
  • 3.1.4 Definition of spacecraft health management

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