Modern space and satellite platforms rely on high-performance embedded compute for onboard processing, control, communication, and payload management. Applications such as Earth observation, telemetry, payload aggregation, and edge analytics demand compact, power-efficient systems that operate reliably in harsh orbital environments.
ZU19/ZU17/ZU11 Zynq UltraScale+ MPSoC-based System on Modules combine FPGA fabric with heterogeneous ARM processing in a compact form factor, enabling real-time acceleration in programmable logic alongside software execution. This architecture supports efficient workload partitioning within the strict power, size, and weight constraints of satellite designs.
A US-based space systems integrator developing satellite subsystems for Low Earth Orbit (LEO) missions was looking for a compact, high-performance embedded compute platform for onboard processing and control. The system was intended for deployment in a ~500 km orbital altitude, with long mission duration and limited access for post-deployment maintenance.
The customer required a proven, flight-ready solution that could be integrated into their existing satellite architecture with minimal design risk and long-term operational reliability.
The customer required a compact, high-performance embedded compute platform capable of reliable long-term operation in a Low Earth Orbit environment at approximately 500 km altitude. The solution needed to tolerate radiation effects without relying on radiation-hardened components or conformal coating, while remaining compatible with a system-level mechanical shielding approach. Additional requirements included low power consumption, deterministic real-time processing, and mechanical robustness suitable for integration within constrained satellite enclosures.
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