توضیحاتی در مورد کتاب a COMBINED DATA AND POWER MANAGEMENT INFRASTRUCTURE : for small satellites.
نام کتاب : a COMBINED DATA AND POWER MANAGEMENT INFRASTRUCTURE : for small satellites.
ویرایش : 2 ed.
عنوان ترجمه شده به فارسی : یک زیرساخت ترکیبی داده و مدیریت نیرو: برای ماهواره های کوچک.
سری :
ناشر : SPRINGER-VERLAG BERLIN AN
سال نشر : 2022
تعداد صفحات : [459]
ISBN (شابک) : 9783662640524 , 366264052X
زبان کتاب : English
فرمت کتاب : pdf
حجم کتاب : 20 Mb
بعد از تکمیل فرایند پرداخت لینک دانلود کتاب ارائه خواهد شد. درصورت ثبت نام و ورود به حساب کاربری خود قادر خواهید بود لیست کتاب های خریداری شده را مشاهده فرمایید.
فهرست مطالب :
Foreword by Robin Biesbroek
Foreword by Ana Ambrosio
Foreword by Olivier L. de Weck
Foreword by René Laufer
Foreword by Peter Martinez
Preface
Donation for Life
Contents
List of Abbreviations
1 System Design Concept
1.1 Introduction
1.2 The Onboard Computer Concept
1.3 The PCDU with Enhanced Functionality
1.4 CPU-Board Reconfiguration Control
1.4.1 Component Functions During Failure Handling
1.4.2 A Combined Controller for PCDU and CPU FDIR
1.4.3 Failure Management with the Combined-Controller
1.4.4 Advantages of the Combined-Controller Approach
1.5 CDPI Software Functions
1.5.1 Software Initialization
1.5.2 SpaceWire Network Initialization and FDIR
1.5.3 Remote-Board Reconfiguration Management
1.6 Firmware Functions
1.6.1 Pulse per Second Signal Management
1.6.2 I/O-Board Interface Operation and Group Tailoring
1.6.3 Ground/Space Communication
1.7 Board Identification
1.8 Completeness of System Architecture
1.9 Outlook for Future Missions
2 OBC CPU-Boards
2.1 Introduction
2.2 GR712RC-SBC
2.2.1 Board Block Diagram
2.2.2 Processor
2.2.3 Memory
2.2.4 Interface Circuits
2.2.5 Auxiliary Circuits
2.2.6 Mechanical Layout and Constraints
2.2.7 PCB Design and Constraints
2.2.8 Housing and Connectors
2.2.9 Components
3 OBC Periphery Boards
3.1 Common Design for SpaceWire Routers, I/O and CCSDS-Boards
3.2 OBC Periphery Boards Overview
3.3 FPGA-Mezzanine
3.3.1 FPGA
3.3.2 Memory
3.3.3 FPGA Configuration
3.4 Carrier
3.4.1 JTAG
3.4.2 Configurable IO
3.4.3 SpaceWire
3.4.4 Ethernet
3.5 System Architecture
3.5.1 Board Implementation
3.5.2 System Grounding
3.5.3 Power Budget
3.5.4 Physical Structure
3.5.5 Loki-Board IO Connectors
3.5.6 Loki-Board Radiation Characteristic
3.5.7 Loki-Board Temperature Limits
4 SpaceWire Router Boards
4.1 SpaceWire Routers for Ground and Flight
4.2 General Router Functions
4.3 Router Board Structure
4.4 Peripherals
4.4.1 Peripheral Identification & Configuration (PID)
4.4.2 Memory and Applications
4.4.3 SpaceWire Ports
4.4.4 SpaceWire-Ethernet Bridge
4.4.5 FPGA Resources
4.4.6 Configuration
4.4.7 PPS Interfaces
4.5 Router-Board Programmers Model
4.5.1 RMAP0
4.5.2 Router Configuration Space
4.5.3 Port0 RMAP SpaceWire Codec
4.5.4 Port0 RMAP PPS
4.5.5 MRAM
4.5.6 Ethernet
5 I/O-Boards
5.1 General I/O-Board Functions
5.2 I/O Board Structure
5.3 Memory and Applications
5.4 Peripherals
5.4.1 I/O-Board Internal Router
5.4.2 SpaceWire Ports
5.4.3 UART Interfaces
5.4.4 GPIO Interfaces
5.5 I/O Board Programmers Model
5.5.1 RMAP0
5.5.2 Router Configuration Space
5.5.3 SpaceWire Codec
5.5.4 MRAM
5.5.5 Configurable I/O Interfaces
5.5.6 UART
5.5.7 GPIO
6 CCSDS Decoder/Encoder Boards
6.1 Introduction
6.2 CCSDS-Board Hardware
6.2.1 Onboard Memory
6.2.2 Peripherals
6.2.3 Memory
6.2.4 FPGA Resources
6.2.5 Configuration
6.3 Functional Overview
6.3.1 Interfaces
6.3.2 Command Link Control Word Coupling
6.3.3 Clock and Reset
6.3.4 Performance
6.3.5 Error Mitigating Strategy
6.3.6 SpaceWire Link Interfaces
6.3.7 On-Chip Memory
6.3.8 Signal Overview
6.3.9 Telemetry Encoder Functional Overview
6.3.10 Telecommand Decoder Functional Overview
6.4 Telemetry Encoder
6.4.1 Layers
6.4.2 Data Link Protocol Sub-layer
6.4.3 Synchronization and Channel Coding Sub-layer
6.4.4 Physical Layer
6.4.5 Connectivity
6.4.6 Operation
6.4.7 Registers
6.4.8 Signal Definitions and Reset Values
6.4.9 TM Encoder—Virtual Channel Generation
6.4.10 TM Encoder—Descriptor
6.4.11 TM Encoder—Virtual Channel Generation Function Input Interface
6.5 TC Decoder—Flight Software Commands
6.5.1 Overview
6.5.2 Waveforms
6.5.3 Coding Layer (CL)
6.5.4 Transmission
6.5.5 Relationship Between Buffers and FIFOs
6.5.6 Command Link Control Word Interface (CLCW)
6.5.7 Configuration Interface (AMBA AHB Slave)
6.5.8 Interrupts
6.5.9 Registers
6.5.10 Signal Definitions and Reset Values
6.6 TC Decoder—High Priority Commands
6.6.1 Overview
6.6.2 Operation
6.6.3 Telecommand Transfer Frame Format—Hardware Commands
6.6.4 Signal Definitions and Reset Values
6.7 SpaceWire Interface with RMAP Target
6.8 JTAG Debug Interface
6.9 Diverse Features
6.10 CCSDS Processor Spacecraft Specific Configuration
7 Integrated Mass Memory Unit
7.1 General
7.2 Introduction
7.3 System Overview with Peripherals
7.4 Mass Memory Handling
7.4.1 Partition Configuration
7.4.2 Memory Recovery
7.4.3 SpaceWire RMAP Implementation
7.5 Memory Mapping
7.6 Interrupt Sources
7.7 Electrical Characteristics
7.7.1 Connectors
7.7.2 Power Consumption
7.8 Mechanical Characteristics
7.9 Radiation Hardness Characteristics
8 OBC Module and Cassette Concept
8.1 OBC-Housing Basics
8.1.1 The Different Boards of the OBC
8.1.2 Concept of the Cassettes
8.1.3 The OBC as Stacked Cassettes
8.1.4 Mount Points of the OBC
8.1.5 Internal Harness Basics
8.2 Mechanical Design of the Cassettes
8.2.1 Design Concept
8.2.2 Individual Cassette Design
8.3 Summary
9 OBC Internal Harness
9.1 Internal Harness Overview
9.1.1 The SpaceWire Harness
9.1.2 The Power Harness
9.1.3 CLCW Interconnects
9.1.4 Pulse Line Connections
9.1.5 JTAG Interfaces
9.1.6 Crypto-Key Load Interfaces
9.2 Interfaces Per OBC Subunit
9.3 Remote Board Nominal/Redundant Identification
10 Board Interconnects to Cassettes
10.1 Introduction
10.2 Flex-PCBs Model to Market
10.3 Router-Board Flex in Detail
10.4 I/O-Cassette Flex Overview
10.5 CCSDS-Cassette Flex Overview
11 Modular Power-Boards
11.1 Introduction
11.2 Mechanical Concept
11.3 Electrical Concept
11.4 Thermal Concept
11.5 The DC/DC Converters
11.5.1 VPT Main Converter
11.5.2 Intersil Converter
11.6 MPB Combined Efficiency
11.7 PCB Layout
11.8 MPB Schematic Design
11.9 MPB Variants
12 OBC Thermal Analysis
12.1 Introduction
12.1.1 Geometrical Mathematical Model of the Housing
12.1.2 Dissipation Points: Router Board
12.1.3 Dissipation Points: I/O-Board
12.1.4 Dissipation Points: CCSDS-Board
12.1.5 Dissipation Points: MMU and MPB
12.1.6 Dissipation Points: CPU-Board and MPB
12.1.7 Summary of Dissipation Values
12.2 Assumptions
12.2.1 Components
12.2.2 Environment
12.3 Results
12.3.1 Case 01
12.3.2 Case 02
12.4 OBC Housing Material Properties
13 Power Control and Distribution Unit
13.1 Introduction
13.2 The PCDU in a Typical Power Supply Subsystem
13.3 PCDU Unit Design Overview
13.3.1 PCDU Interfaces
13.3.2 PCDU Command Concept
13.4 Boot-Up Sequence of the PCDU and PCDU Modes
13.5 Power Control and Distribution Functions
13.6 PCDU Specific Functions in the CDPI Architecture
13.6.1 Analog Data Handling Concept
13.6.2 Reconfiguration Logic for the OBC
13.6.3 Reconfiguration Functionality for the Spacecraft
13.7 Diverse PCDU Functions
13.7.1 Launcher Separation Detection
13.7.2 Control and Monitoring of Solar Panel Deployment (Optional)
13.7.3 Control of the Payload Data Transmission Subsystem Power
13.7.4 History Log Function
13.7.5 Time Synchronization Between Internal Controllers
13.7.6 Overvoltage Protection
13.8 PCDU Environmental Qualification Characteristics
13.8.1 Thermal-Vacuum Limits
13.8.2 Radiation Limits
13.8.3 Vibration Limits
13.9 List of Connectors
13.10 PCDU Commands Overview
13.11 The PCDU and Electric Propulsion Systems
14 CDPI Functional Testing
14.1 Introduction
14.2 Test Scope
14.3 Test Conditions
14.4 Test Plan, Test Procedures and Setups
14.4.1 Power-Board Tests
14.4.2 CPU-Board Tests
14.4.3 SpaceWire RTR-Board Tests
14.4.4 I/O-Boards Tests
14.4.5 CCSDS-Boards Tests
14.4.6 MMU Tests
14.4.7 PCDU Tests
14.4.8 OBC Subsystem Tests
14.4.9 CDPI Reconfiguration Tests
14.5 Test Execution on STB
14.5.1 Satellite Testbed Infrastructure
14.5.2 Typical Test Stages on a Satellite Testbed
14.6 Test Execution on FlatSat
15 OBC Mechanical Qualification
15.1 Introduction
15.2 Structural Analysis
15.3 Determination of Eigenfrequencies
15.4 Vibration Testing
15.5 Shock Testing
15.6 Mechanical Properties
16 Example Missions
16.1 ClearSpace “ADRIOS CS-1”
16.1.1 The Motivation
16.1.2 The ClearSpace-1 Service to ESA
16.1.3 The Target
16.1.4 The Mission
16.1.5 The ClearSpace-1 Servicer
16.2 Thailand Space Program and FLP2
16.3 Stuttgart University “Flying Laptop”
16.3.1 Technology and Payloads
16.3.2 Satellite Attitude Control System
16.3.3 Satellite Electrical Architecture and Block Diagram
17 Annexes and Data Sheets
17.1 GR712RC-SBC Interface Board
17.1.1 Power Circuits
17.1.2 JTAG (FTDI USB) Interface
17.1.3 Interface Configuration Logic/Circuits & GPIO/GPIN
17.1.4 Mechanical Layout, Design and Constraints
17.1.5 List of Connectors—IF-Board
17.1.6 List of Oscillators, Switches and LED's—IF-Board
17.1.7 List of Switches and LED's—IF-Board
17.2 CCSDS Conventions
17.2.1 CCSDS Field Definitions
17.2.2 Galois Field
17.2.3 Telemetry Transfer Frame Format
17.2.4 Reed-Solomon Encoder Data Format
17.2.5 Attached Synchronization Marker
17.2.6 Telecommand Transfer Frame Format
17.2.7 Command Link Control Word
17.2.8 Space Packet
17.2.9 Asynchronous Bit Serial Data Format
17.2.10 SpaceWire Remote Memory Access Protocol (RMAP)
17.2.11 Command Link Control Word Interface (CLCW)
17.2.12 Waveform Formats
17.2.13 Selected TM Encoder Registers
17.2.14 TM Encoder—Virtual Channel Generation Registers
17.2.15 Selected TC Decoder Registers
17.3 OBC Unit CAD Drawing
17.4 OBC External Connectors
17.4.1 CPU-Board
17.4.2 MMU-Board
17.4.3 CCSDS-Board
17.4.4 SpW Router-Board
17.4.5 I/O-Board
17.5 PCDU Unit CAD Drawing
17.6 PCDU Unit Connector Pin Allocations
17.7 PCDU Switch and Fuse Allocation to Spacecraft Equipment
References
Index