iADCS200
AAC Clyde Space
The iADCS200 is an Attitude Determination and Control System (ADCS) designed for small satellites.
Key figurescomparable across the catalogue
- Mass
- 0.09 kg
- Power
- 1.5 W
- Largest dimension
- 90 mm
- TRL
- 9
Normalised to common units so this product can be compared with others in its category. The supplier's own wording is below.
As published by the supplier
- 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 provided page only lists the name ‘iADCS200’ and links to other related products. It does not offer a detailed description, features, configurations, applications, or flight heritage for the iADCS200 itself. The other products mentioned are: AAC SpaceQuest ANT-GPS-Series Antenna (space qualified L-band patch antenna for MicroSats and SmallSats), AAC SpaceQuest GNSS-701 (compact satellite GNSS receiver), AAC Hyperion iADCS400 (fully autonomous ADCS for 6U CubeSats or larger), AAC SpaceQuest MAG-3 (three-axis satellite magnetometer), AAC Hyperion MM200 (high precision magnetometer), AAC Hyperion MTQ800 (small satellite precision magnetorquers), AAC Hyperion PG400 GYROSCOPE (high-performance gyroscope with RS422 interface), AAC Hyperion RW222 (next-generation high-performance reaction wheels), AAC Hyperion RW400 (high-performance reaction wheels), AAC Hyperion ST200 (CubeSat star tracker for pico- and nano-satellites), AAC Hyperion ST400 (powerful star tracker for microsatellites), and Trillian-1 (high reliability reaction wheel for Small Satellite missions).
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.