CubeSat ADCS Subsystem
Attitude Determination and Control System (ADCS) for 1U, 3U, and 6U CubeSats — provides precise orientation and stabilization for space missions.
Technical specifications
- Supported form factors
- 1U, 3U, 6U CubeSat
- Function
- Attitude determination and control
- Test facilities
- ADCS simulator, air-bearing testbed, Helmholtz cage, star tracker testbed
About
NBSpace’s ADCS Subsystem delivers precision attitude determination and control for 1U, 3U, and 6U CubeSat platforms. The system is designed to provide reliable orientation and stabilization for space missions requiring pointing accuracy — such as Earth observation, remote sensing, and communications payloads. Available in configurations tailored to each form factor, the ADCS supports mission-critical stability throughout the mission lifecycle. NBSpace develops the system in-house, controlling quality from design through manufacturing and test using their on-site ADCS simulator, air-bearing testbed, Helmholtz cage, and star tracker testbed.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.