These 1/2U Attitude Determination and Control Systems feature 3 reaction wheels, a 3-axis magnetometer, 2 IR Earth Horizon Sensors (IR EHS) or 2 Star Trackers, 3 electromagnets and an ADACS computer for a stand-alone, Plug-and-Play attitude control system for small satellites.
- Pointing control of 0.1 degrees, with Space Sextant, or 1 degree with IR Earth Horizon Sensors
- 100 x 100 x 52 mm
- 694 g
- 1.13 W nominal nadir pointing, 3.2 W peak slew @ 5 V
- Interfaces via RS232 or SCI/UART @ 3.3 V