CAVU Aerospace UK

OBC, Onboard Computer, OBC-PolarFire Space VPX, Satellite OBC, Satellite Onboard Computer, Microchip, flash-based FPGA architecture, Command and Data Handling

CoaXPress OnBoard Recorder

DESCRIPTION

OBR handles high data rate missions by combining high-speed CoaXPress acquisition with FPGA-based deterministic processing, a large ECC-protected burst buffer and high-throughput multi-drive storage. The philosophy is straightforward: Capture at the speed of the sensor, Buffer without losing data, Store continuously & Protect the data throughout the pipeline. Built around the Microchip PolarFire SoC, the architecture provides a flexible platform that can evolve from today’s CXP-based imaging systems toward future high-speed custom serial payload interfaces.

Microchip, OBC, Onboard Computer, Satellite OBC, Satellite Onboard Computer, SBC

KEY FEATURES

  • Processor: Microchip PolarFire SoC MPFS460T
  • High-speed inputs: 8 × configurable SERDES
  • Supported interfaces: CXP-3 / CXP-6 / CXP-12 / custom serial
  • Design-point input processing: 25 Gbps
  • Representative payload rate: 23.1 Gbps
  • Burst buffer: 128 Gbit / 16 GB
  • Total memory architecture: 144 Gbit
  • Memory protection: ECC
  • Sustained DDR4 bandwidth: 12.8 GB/s
  • NVMe storage: 2 × U.2, PCIe Gen2 x2
  • SATA storage: 4 × U.2 SATA III
  • Aggregate storage write: 3.5 GB/s
  • High-Capacity Mass Storage: 2 × U.2 NVMe
  • Example 5-second / 25 Gbps burst: 125 Gbit / ~15.6 GB

CoaXPress

CoaXPress originated as a high-speed imaging interface and is particularly well suited to applications where large volumes of camera data need to move with predictable latency. The interface supports high-speed downstream data together with lower-speed control communication. CoaXPress can also carry power over coax in appropriate implementations. For spacecraft applications, the most interesting characteristic is its ability to provide a simple, scalable physical interface for very high-rate imaging data. With CXP-12 providing up to 12.5 Gbps per connection, multiple links can be aggregated to support substantially higher payload data rates. For a spacecraft carrying several cameras, this opens an interesting architecture.

PRODUCT DOCUMENTS

  • Failure Modes, Effects, and Criticality Analysis (FMECA)
  • Reliability Analysis Report
  • Radiation Analysis Report
  • Safety Assurance Plan
  • Fault Tree Analysis (FTA)
  • Single Point Failure Analysis (SPFA)
  • Worst Case Analysis (WCA)
  • Derating Analysis Report
  • Availability Analysis Report
  • Mechanical Analysis Report
  • Maintainability Analysis Report
  • Fault Detection, Isolation, and Recovery (FDIR)
  • Qualification Test Plan (QTP)
  • Environmental Test Reports, TVAC, Vib.
  • EMC/EMI Test Report
  • Radiation Test Report
  • Operational Risk Assessment (ORA)
  • Critical Items List (CIL)
  • Materials, Processes, and Mechanical Parts List (MPMPL)
  • Product Assurance Plan (PAP)
  • Configuration Item Data List (CIDL)
  • End Item Data Package (EIDP)
  • As-Built Configuration List (ABCL)