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Spacecraft power system technologies 版權信息
- ISBN：9787568290630
- 條形碼：9787568290630 ; 978-7-5682-9063-0
- 裝幀：一般膠版紙
- 冊數：暫無
- 重量：暫無
- 所屬分類：>>
Spacecraft power system technologies 內容簡介
This book provides an introduction to the main design principles， methods， proceclurcs，and development trends in spacecraft power systems. It is divided into nine chapters，the first of which covers the classification and main components of primary power system design and power distribution system design. In turn， Chapters 2 to 4 t'ocus on the spacecraft power system design experience and review the latest typical design cascs concerning spacecraft power systems in China. More specifically， these chapters also introduce readers to the topological structure and key technologies used in spacecraft power systems. Chapters 5 to 7 address power system reliability and safety design，risk analysis and control， and inorbit management in China's spacecraft engineering projects. The book's closing chapters provide essential information on new power systems and technologies， such as space nuclear power， micro- and nano-satellite power systems， and space energy interconnection systems. An outlook on future development trends rounds out the coverage.
Spacecraft power system technologies 目錄
1 Introduction
1．1 Definitions and Functions
1．2 Classification and Composition
1．2．1 Classification
1．2．2 Composition
1．3 Primary Power Subsystem
1．3．1 Power Generation Technologies
1．3．2 Power Storage Technology
1．3．3 Power Control Technology
1．4 System Circuit Subsystem （SCS）
1．4．1 Power Distribution Architecture
1．4．2 Tasks and Configuration of SCS
1．4．3 Overcurrent Protection Technology
1．5 Development Process of Spacecraft Power System
1．5．1 Development Phases
1．5．2 Development Process
1．6 Power System Evaluation
1．7 Development of Spacecraft Power System in China
1．7．1 Development of Spacecraft Power System Technology
1．7．2 Development of Spacecraft Power Distribution
Technology and SCS Technology
References
2 Design of Primary Power Subsystem
2．1 Design Basis and Constraints
2．1．1 Space Environment and Its Effects
2．1．2 Flight Mission
2．1．3 Mutual Constraints in the Design of Spacecraft Power System
2．1．4 Flight Procedure
2．1．5 Lighting Conditions
2．1．6 Payload Configuration and Load Characteristics
2．2 Power System Topology
2．2．1 Bus Voltage
2．2．2 Bus Configuration
2．2．3 Power Regulation of Solar Arrays
2．2．4 Energy Transfer Method
2．2．5 Bus Voltage Regulation Methods
2．2．6 Installation of Solar Array
2．3 Design and Calculation of Power System
2．3．1 Solar Array
2．3．2 Battery Pack
2．3．3 Power Control Unit （PCU）
2．3．4 Energy Balance Analysis
References
3 Design of System Circuit Subsystem （SCS）
3．1 General
3．2 Working Environment and Constraints
3．2．1 Electromagnetic Environment
3．2．2 Mechanical Environment
3．2．3 Thermal Environment
3．2．4 Space Environment
3．2．5 Other Environments
3．3 System Design
3．3．1 Design of Load Power Priority
3．3．2 Design of Distribution Bus System
3．3．3 Design of Distribution Bus Control
3．3．4 Bus Protection Design
3．4 Design of Grounding and Lapping
3．4．1 Design of Grounding System
3．4．2 Design of Spacecraft Grounding and Lapping
3．4．3 Design Examples of Spacecraft Grounding and Lapping
3．5 Design of System Circuit Interfaces
3．5．1 General
3．5．2 Design of Iter face Between Satellite （Spacecraft）and Rocket
3．5．3 Design of Interface Between Satellite （Spacecraft）and Ground
3．5．4 Design of Other Key Interfaces
3．6 Design of System Circuit
3．6．1 Power Distribution Unit （PDU）
……
4 Design Example of Power System
5 Reliability and Safety Design for Power System
6 Analysis and Control of Technical Risks in Power System
7 Power System Testing and Environment Experiments
8 Autonomous Management of Power System
9 Further Space Task demands and Power System Development
Trends
1．1 Definitions and Functions
1．2 Classification and Composition
1．2．1 Classification
1．2．2 Composition
1．3 Primary Power Subsystem
1．3．1 Power Generation Technologies
1．3．2 Power Storage Technology
1．3．3 Power Control Technology
1．4 System Circuit Subsystem （SCS）
1．4．1 Power Distribution Architecture
1．4．2 Tasks and Configuration of SCS
1．4．3 Overcurrent Protection Technology
1．5 Development Process of Spacecraft Power System
1．5．1 Development Phases
1．5．2 Development Process
1．6 Power System Evaluation
1．7 Development of Spacecraft Power System in China
1．7．1 Development of Spacecraft Power System Technology
1．7．2 Development of Spacecraft Power Distribution
Technology and SCS Technology
References
2 Design of Primary Power Subsystem
2．1 Design Basis and Constraints
2．1．1 Space Environment and Its Effects
2．1．2 Flight Mission
2．1．3 Mutual Constraints in the Design of Spacecraft Power System
2．1．4 Flight Procedure
2．1．5 Lighting Conditions
2．1．6 Payload Configuration and Load Characteristics
2．2 Power System Topology
2．2．1 Bus Voltage
2．2．2 Bus Configuration
2．2．3 Power Regulation of Solar Arrays
2．2．4 Energy Transfer Method
2．2．5 Bus Voltage Regulation Methods
2．2．6 Installation of Solar Array
2．3 Design and Calculation of Power System
2．3．1 Solar Array
2．3．2 Battery Pack
2．3．3 Power Control Unit （PCU）
2．3．4 Energy Balance Analysis
References
3 Design of System Circuit Subsystem （SCS）
3．1 General
3．2 Working Environment and Constraints
3．2．1 Electromagnetic Environment
3．2．2 Mechanical Environment
3．2．3 Thermal Environment
3．2．4 Space Environment
3．2．5 Other Environments
3．3 System Design
3．3．1 Design of Load Power Priority
3．3．2 Design of Distribution Bus System
3．3．3 Design of Distribution Bus Control
3．3．4 Bus Protection Design
3．4 Design of Grounding and Lapping
3．4．1 Design of Grounding System
3．4．2 Design of Spacecraft Grounding and Lapping
3．4．3 Design Examples of Spacecraft Grounding and Lapping
3．5 Design of System Circuit Interfaces
3．5．1 General
3．5．2 Design of Iter face Between Satellite （Spacecraft）and Rocket
3．5．3 Design of Interface Between Satellite （Spacecraft）and Ground
3．5．4 Design of Other Key Interfaces
3．6 Design of System Circuit
3．6．1 Power Distribution Unit （PDU）
……
4 Design Example of Power System
5 Reliability and Safety Design for Power System
6 Analysis and Control of Technical Risks in Power System
7 Power System Testing and Environment Experiments
8 Autonomous Management of Power System
9 Further Space Task demands and Power System Development
Trends
展開全部
Spacecraft power system technologies 作者簡介
Qi Chen， Ph.D.， researcher， born in Luoyang， Henan Province in July 1974. He is now the Deputy Director of Institute of Spacecraft System Engineering， China Academy of Space Technology， engaged in the design of spacecraft power supply system and the development planning of space energy technology. He is also a member of the Space Energy Committee， Chinese Academy of Astronautics. As chief designer， he pre-sided over the development of more than ten satellite power subsystems， represented by HY-2 and ZY Series.He took charge of and accomplished a number of civil aerospace and equipment pre-research projects as pro-ject leader. In 2014， he won the China Space Fund Award. In 2015， he was honored the first prize of National Defense Science and Technology Award. In 2016， he received the second prize of National Scientific and Technological Progress Award. He has translated one book， published more than 40 papers in Chinese and international academic journals， and owned more than ten authorized patents.Zlugang Liu， Ph.D.， researcher， born in Changsha，Hunan Province in June 1982. Currently， he is the Vice Director of Electronic Information Division， Institute of Spacecraft System Engineering， China Academy of Space Technology. He is mainly engaged in the design of spacecraft power supply and distribution system， the energy management of high-power spacecraft， the development of near-field wireless energy transfer tech-nology. He has participated in the development of power supply and distribution subsystems of Chang'e-5 fiight tester， Chang'e-5 and Mars probe. He presided over a number of aerospace pre-research technology projects.He has published more than 20 academic papers and owned more than ten authorized China nationalinvention patents and seven software copyrights.Xiaofeng Zhang， Master， Senior Engineer. He was born in Xingtai， Hebei Province， in June 1984. Currently， he is designer of spacecraft electrical power system，with Institute of Spacecraft System Engineering，China Academy of Space Technology. He is mainly engaged in the overall design of spacecraft power supply system， space distributed energy control and interconnection. He has participated in the development of power subsystems for navigation satellite. He presided over and participated in a number of civil aerospace and equipment pre-research projects. He has published more than 20 papers in Chinese and inter-national academic journals. Liying Zhu， Ph.D.， senior engineer， born in Tangshan，Hebei Province， in June 1985. Currently， she is working in Beijing Institute of Spacecraft System Engineering， China Academy of Space Technology. She is mainly engaged in the design of spacecraft power supply and distribution system， high-power spacecraft energy management， near-field wireless energy transfer technology. She has participated in"YG-1" "BD-3." She has presided over a National Natural Science Foundation of China and participated in equipment prefabrication sharing technology and special technologies for pre-research projects in the aerospace field. She has published more than 30 papers in Chinese and international academic journals， and authorized more than five national invention patents.
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