Image processing computer for satellites compliant with the 3U OpenVPX standard.
A satellite image processing computer compatible with the 3U OpenVPX standard. It features a 3U VPX single-board computer and a reconfigurable FPGA for high bandwidth applications. Additionally, it is capable of real-time 12-bit compression.
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basic information
The main specifications are as follows: - FPGA: Xilinx Kintex UltraScale * LUTs = 221k * FFs = 663k * DSPs = 2760 * BRAM = 38.0Mb - Memory: DDR3 SDRAM, 16GB; MRAM, 64MB; Flash, 64GB to 128GB; ADC - Interface: 12 - LVDS Input pairs; 12 - LVDS Output pairs; 16 - GPIO (digital, single-ended); 8 - RS422 Input pairs; 8 - RS422 Output pairs; 4 to 6 PCIe Input/Output; 8 Channel Analog - Debug Interface: JTAG, USB - Operating Temperature Range: -40℃ to +65℃ - Radiation Resistance: TID >100 kRad(Si); No SEFI - Dimensions: 201 x 150 x 112mm SDU and EM are also available.
Price information
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Delivery Time
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Applications/Examples of results
It can be applied to artificial satellites that require image processing in orbit.
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.