Miniature and lightweight GPS receivers for ultra-small satellites, CubeSats, etc.
A small, lightweight GPS receiver designed to fit the dimensions of ultra-small satellites, CubeSats, etc. It uses a dual Cortex A9 core microprocessor and a reconfigurable FPGA (Zynq-7020 and ProASIC3000).
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basic information
The main specifications of the µGPS-C receiver are as follows: 1. Position accuracy: <10m 2. Velocity accuracy: <5cm/s 3. Measurement data rate: 1sec 4. Position data rate: every 10sec 5. Operating frequency: L1 C/A with options for L2C, L5, P(Y), M-Codes 6. Weight: 1.5kg 7. Dimensions: 10x10x8cm 8. Power consumption: approximately 8W (excluding LNA) 9. Operating temperature range: -20℃ to +65℃ 10. Input voltage: +28V 11. Radiation tolerance (TID): 30krads (Si)
Price information
Please contact us regarding the price.
Delivery Time
※Please inquire about the delivery date.
Applications/Examples of results
GPS receiver that can be used for ultra-small satellites such as CubeSats.
Company information
The Advanced Technology Research Institute is an engineering company that supports space development and utilization, including rockets and artificial satellites, in Japan and around the world. We conduct a wide range of activities from the design and development of space systems, subsystems, and components for satellites and rockets, both small and large, to the sale of overseas space equipment. Additionally, we sell solar cells for space and ground use, and we design and develop solar cell panels for space as well as sell solar power generation modules and systems for ground use. For small satellites, including CubeSats, we provide system development from 1U to 12U, offer bus components, design and develop bus equipment, assemble satellites, and conduct integration and testing of satellites, including payloads. We also design, develop, and sell small electric propulsion systems for CubeSats and small satellites.
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