Cutting-Edge Satellite Technology
The HUNITY satellite integrates multiple sophisticated subsystems working together to enable scientific research and technology demonstration in space.


Electric Power System (EPS)
- RP2040 microcontroller
- 3.3 V regulated voltage generation
- 6 channel MPPT (solar maximum power point tracking circuit)
- Incoming and consumed power (current and voltage) telemetry


On-Board Computer (OBC)
- RP2040 microcontroller
- On-board systems data collection and storage
- Task scheduling
- Generate normal telemetry


Battery + Sensor Data Logger (BAT)
- RP2040 microcontroller
- Battery protection
- Sensor data acquisition
- Orientation determination
- Satellite position calculation SGP4 algorithm


GPS + RadNano (GRS)
- RP2040 microcontroller
- Space qualified GPS
- 27G Radnano total ionizing radiation meter


Communication (COM)
- RP2040 microcontroller
- Stand-alone power supply
- Reprogramming of images/subsystems
- 437,390 MHz (12.5 kHz UL, 20 kHz DL)


Active Magnetic Orientation Control (ACMAG)
- RP2040 microcontroller
- Three-axis electrical coils


Active Rotating Mass principle Orientation Control (ACMOT)
- RP2040 microcontroller
- Reluctance motor
- Operates along 3 axes


Sun and Horizon Sensor (SUN)
- 16x12 matrix far infrared sensor
- 4 directions, per direction 110° × 75° field of view


Pi Pico and FPGA experiment (PIF)
- Science promotion with Pi Pico
- FPGA IC testing


Solar Cell Life Tester
- Azurspace GaAs (3 and 4 layers, Germany)
- YimSpace GaAs (3 layers, China)
- Anysolar Si mono (1 layer, South Korea)