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Attitude and Orientation Control System [AOCS]

Nanosatellite Attitude Control

  • Purpose: The unit is designed for controlling the external magnetic coils integrated in solar panels.
  • Year of release: 2016
  • Guaranteed service life (years): 1 year
  • Estimated production / delivery time (months): 6
  • Flight qualification of the product: No
  • Possibility to adapt the product to customer requirements: Yes
ParameterValue
Channel number2
Maximum current3 А
Pick PWM power3 W
PWM voltage3.3 - 15 V
PWM frequency30 - 30000 Hz
PWM resolution8 bit

Features:

  • independent PWM signal generation for two axis;
  • connection of solar panels through clamping connector;
  • connection up to 4 magnetic coils in solar panels;
  • bus options: PC104 or original.