The NANOadcs from SkyLabs d.o.o. is a high-performance guidance, navigation, and control platform designed as a complete Attitude Determination and Control System (ADCS) for small satellites. Featuring a compact and highly integrated architecture, the system incorporates a fault-tolerant 32-bit RISC-V onboard computer that executes advanced GNC algorithms, enabling precise attitude determination and high-accuracy pointing for modern satellite missions. This integrated ADCS solution combines a multi-constellation GNSS receiver with onboard sensors such as a magnetometer and gyroscope, providing accurate real-time attitude and position data.

It includes configurable, LCL-protected power channels supporting multiple voltage levels (3.3 V, 5 V, 12 V, and 18 V) and operates across a wide input voltage range of 5 V to 28 V, ensuring flexible power management and compatibility with various satellite platforms. The system supports a comprehensive set of communication and control interfaces including RS422, CAN, UART, I2C, analog inputs and PWM outputs, enabling seamless integration with actuators and other spacecraft subsystems.

Developed as a fully European solution in collaboration with Indra Deimos, NANOadcs enhances system resilience, security and innovation while maintaining high reliability in space environments. Compact and robust, the NANOadcs is ideal for nanosatellites and small satellite missions requiring precise attitude control, efficient subsystem integration and dependable performance across a wide range of orbital applications.

Key features

Built-in NANOhpm
Interface
- Redundant CAN
- for TM/TC
Integrated On-Board sensors
- GNSS receiver,
- magnetometer, gyro
Configurable LCL protected power channels
- 3.3V, 5V, 12V, or 18V
Sensors and actuators interfaces
- 5x RS422, 1xCAN,4x UARTs, I2C,
- 12x Analog TIA&NTC,
- 3x Current ctrl. Full-bridge PWMs, 1PPS I/O
Wide input power range
- 5V - 28 V

Datasheet for NANOadcs - Attitude determination and control system by SkyLabs

Datasheet