Description
Attitude Determination Control System – responsible for satelitte’s on-orbit steering.
Based on:
- 2x 3 axis Gyroscope
- 2x 3 axis Accelerometer
- 2x 3 axis Magnetometer
- 3x Magnetorquers
- 2D fine sun sensor
Attitude Determination and Control System
4 500.00 $
Attitude Determination Control System – responsible for satelitte’s on-orbit steering.
Features
- Orientation accuracy: ~2deg
- Max power: 0.9 W
- Power supply: 3.3 V, 12V
- High power computation unit (ARM Cortex M4 @ 100MHz)
- SGP4 / SGD4 propagator implemented
- IGRF 12 geomagnetic model implemented
- RTC on board available
- Quaternion or Euler angles attitude representation
Details
- Orientation accuracy: ~2deg
- Max power: 0.9 W
- Power supply: 3.3 V, 12V
Magnetorquers:
- 3-axis control
- Current consumption: 0.0 – 0.5A per axis
- Manual control possible
Properties
- Mass: 50 g
- Size: 96 x 96 x 1.6 mm3
- Compatible with PC-104 mechanical interface
Tests
- Thermal-vacuum
- Random vibration
- EMC
