Product overview
The computer uses a serial LVDS backplane architecture and allocates resources to provide redundancy for its CPU, interfaces and power supply. Its main/standby operating mode is designed to maintain operation after a failure.
The listed applications include conversion of a manned helicopter to an unmanned platform, coaxial unmanned helicopter development and a UAV platform.
Specifications
| Specification | Value & conditions |
|---|---|
| Redundancy | CPU, interfaces and power supplyImplemented through resource allocation in a main/standby architecture. |
| Design features | Redundant flight control computer; compact format; large storage capacityFeatures stated in the onboard equipment product listing; no quantitative specifications supplied. |
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