🛰️ Satellite Backplane System Architecture
Advanced Hybrid Processing System for Space Applications
System Interface
SRAM
Secondary
Storage
EEPROM
RF
Transceiver
Satellite Backplane
Reconfiguration Handler
Reconfiguration
microprocessor
Configuration
memory
Power Management Module
PMIC
Power Supply
interfaces
SPI
🔧 Hybrid Processing System
FPGA Module
Crypto
Engine
I/O
Interface
Interface
Controller
Analog Compute Module
Analog CIM
cores
Flash
memory
ADC/DAC
PCIe or AXI bus | Processed data bus | Control data bus
SPI/LVDS/UART/I2C
(Reconfigurable bus)
Payload Interface
CubeSat Subsystems
Payload
sensors
Communication
modules
Housekeeping
units
System Status
System Status:
OPERATIONAL
Active Modules:
0
/9
Power Consumption:
75W
Data Throughput:
1.2 Gbps
Temperature:
-15°C