iADCS200
AAC Clyde Space
Integrated Attitude Determination and Control System for 1U-3U CubeSats, combining sensors and actuators in a single compact board.
Technical specifications
- Pointing Accuracy
- ~1° (3σ)
- Attitude Rate
- <0.5°/s
- Sensors
- 3-axis magnetometer, sun sensors, gyroscope
- Actuators
- 3-axis magnetorquers
- Interface
- I2C / CAN
- Supply Voltage
- 3.3 V / 5 V
- Power Consumption
- ~1.5 W
- Operating Temperature
- -40°C to +85°C
- Mass
- ~90 g
- Dimensions
- ~90 x 90 x 16 mm
- Radiation Tolerance
- 10 KRad
- TRL Level
- 9
- Compatible CubeSat Size
- 1U to 3U
- Orbit Support
- LEO
- ADCS Software
- Embedded (EKF-based)
About
The iADCS200 is an integrated ADCS module from AAC Hyperion designed for 1U to 3U CubeSats. It combines a 3-axis magnetometer, sun sensors, gyroscopes, and magnetorquers on a single board with an embedded attitude determination and control processor. This all-in-one approach simplifies system integration and reduces mass and volume. The module provides pointing accuracy suitable for moderate-precision Earth observation and technology demonstration missions.
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.
