Nanosatellite Onboard Computer
Triple-core nanosatellite OBC (AVR + M0 + M4F, 200 MHz, 32 GB microSD, 9-DOF IMU, CAN/I2C/UART/SPI interfaces).
Technical specifications
- Purpose
- Nanosatellite onboard computer — sensor collection, measurement processing, storage, control actuation, telecommand processing, telemetry generation
- Year of release
- 2016
- Guaranteed service life
- 1 year
- Estimated production/delivery time
- 6 months
- Flight qualification
- Not yet flight qualified
- Customization
- Can be adapted to customer requirements
- CPU cores
- AVR, Cortex M0, Cortex M4F (3 cores, 2 independent MCUs)
- Clock frequency
- 8 MHz / 200 MHz
- RTC battery backup
- 5 months
- Storage
- 2 × microSD up to 32 GB (shared access)
- IMU (per set)
- 3-axis magnetometer (4.8 mT range, 16 bit), accelerometer (±2 g, 16 bit), gyroscope (±250 °/s, 16 bit)
- IMU sets
- 2 (redundant)
- Interfaces
- I2C, UART, SGPIO, CAN
- Power monitors
- 5 independent
- Bus interface
- PC104 or original
- TRL
- 6
About
The Nanosatellite Onboard Computer collects information from sensors, processes measurements, stores results, forms control actions, processes telecommands, and generates telemetry packets. It features three CPU cores (AVR, Cortex M0, Cortex M4F) with clock frequencies of 8 and 200 MHz, two independent MCUs with 2 sets of 3-axis accelerometer, gyroscope, and magnetometer, 2 microSD cards with shared access (up to 32 GB each), five independent power monitors, and an RTC with 5-month battery backup. Multiple interfaces include I2C, UART, SGPIO, and CAN. Available with PC104 or original bus. Released in 2016 with a 6-month delivery time.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
