Instrument Control Unit (ICU)

Overview
Instrument thermal control & Payload data processor in single sub-system
KEY FEATURES
Radiation-tolerant components and TID monitoring.
Integrated FPGA co-processing capabilities.
Autonomous thermal management.
Dedicated power distribution and monitoring circuits.
Fault detection, isolation, and recovery (FDIR) capabilities.
Redundant communication interfaces ensuring reliable data transfer.
FUNCTIONS
Real-time data acquisition and processing from sensors, including temperature and radiation sensors.
Autonomous heater control loops based on configurable temperature set points and profiles.
Robust power management and latch-up protection.
Secure firmware updates, remote image management, and rollback mechanisms.
High-precision timing synchronization through onboard RTC.
Housekeeping data collection, logging, and telemetry reporting.
FPGA-based custom computational offloading and acceleration.
INTERFACES & DATA COMMUNICATION
SpaceWire Interfaces: Main and redundant backup interfaces for reliable communication with the OMA subsystem. Main and Redundant communication with the PLHU platform. Main and redundant interfaces for auxiliary camera.
CAN Bus Interfaces: Telemetry and telecommand communication with the PLHU subsystem. Additional redundant CAN interfaces for mission expansion and fault tolerance.
RS422 Interfaces: Multiple RS422 communication channels provided for robust data transfer, subsystem interfacing, and debugging purposes.
Ethernet Interface: Ethernet port dedicated to debugging, software developments, and system diagnostics.
Sensor Interfaces: Integrated radiation-tolerant ADC channels for temperature sensor readings and radiation monitoring.
Heater Control Interfaces: PWM-controlled heater channels with built-in short-circuit and fault detection mechanisms.
Power Interfaces: Dedicated regulated 12V DC power line for the OMA subsystem. Monitored and controlled power rails with independent latch-up protection.
Looking for more information or want to purchase?
Overview
- Name
- Instrument Control Unit (ICU)
- Vendor
- CAVU AEROSPACE
- Subsystem
- CDH Subsystem
- Component Type
- On-Board Computer
- Form Factor
- SmallSat
- Heritage
- Yes
- Average Lead Time
- 4 to 9 months
Vendor Details
- Name
- CAVU AEROSPACE
- Website
- https://CavuAerospace.uk/
- Founded
- 2002
- Summary
- CAVU AEROSPACE is a British manufacturer of satellite & Launch vehicles components. Core Business: On Board Computers Based in Scotland, Stirling University Innovation park. Since 2002 in Aviation & 2017 in Space
Vendor Request for Information Form
Specifications
- Subsystem
- CDH Subsystem
- Component Type
- On-Board Computer
- Form Factor
- SmallSat
- Vendor
- CAVU AEROSPACE
- Dry Mass
- 1.8 kg
- Average Power
- N/A
- Heritage
- Yes
- Status
- In Production

Try Designer
Design, model, and evaluate satellite mission concepts quickly with our software.

CAVU AEROSPACE
CAVU AEROSPACE is a British manufacturer of satellite & Launch vehicles components. Core Business: On Board…
View all products