ISpaceI ADCS — Attitude Determination and Control System
ISpaceI Satellite and Research
Compact ADCS for 1U–3U CubeSats providing three-axis attitude determination and control.
Technical specifications
- Compatible form factors
- 1U, 2U, 3U CubeSat
- Control type
- Three-axis active attitude control
- Integration
- Compatible with ISpaceI OBC and EPS subsystems
- Mounting
- Internal CubeSat frame
- Target orbit
- Low Earth Orbit (LEO)
About
The ISpaceI ADCS (Attitude Determination and Control System) is a flight-ready subsystem designed for 1U to 3U CubeSats, enabling precise orientation management in low Earth orbit. It integrates attitude determination sensors with active control actuators to maintain satellite pointing for payloads, communication antennas, and solar panels.
The system is engineered to operate within the tight mass, volume, and power constraints of nanosatellites while delivering reliable three-axis stabilization. ISpaceI supplies the ADCS as a standalone subsystem or as part of their complete CubeSat integration service, pre-tested and ready for interface with the onboard computer. The design supports standard CubeSat form factors and is compatible with ISpaceI’s EPS and OBC subsystems for fully integrated missions.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.