Nanosatellite Attitude Control
Dual-channel magnetic torquer driver board for nanosatellites, controlling external magnetic coils in solar panels (PWM, 3 W peak, PC104).
Technical specifications
- Purpose
- Controlling external magnetic coils integrated in solar panels for nanosatellite attitude control
- 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
- Channels
- 2 (independent PWM per axis)
- Maximum current per channel
- 3 A
- Peak PWM power
- 3 W
- PWM voltage
- 3.3–15 V
- PWM frequency
- 30–30,000 Hz
- PWM resolution
- 8 bit
- Coil connections
- Up to 4 magnetic coils in solar panels
- Interface
- PC104 or original bus
- TRL
- 6
About
The Nanosatellite Attitude Control unit is a 2-channel PWM driver board designed for controlling external magnetic coils integrated into the solar panels of nanosatellites. It generates independent PWM signals for two axes, supports connection of up to 4 magnetic coils in solar panels, and features 8-bit PWM resolution at 30–30,000 Hz with up to 3 A per channel and 3 W peak power. Available with PC104 or original bus interface. Released in 2016 with a 6-month delivery time.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.