HARDWARE / PRODUCT

Nanosatellite Attitude Control

Glavkosmos
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.

Source: trade.glavkosmos.com ↗