FIRE CONTROL AND FLIGHT GUIDANCE

Guidance core

Seeker fusion, state estimation, proportional navigation and autopilot, implemented in logic and sized for a low-cost interceptor.

5 kHzLOOP RATE

0MEASURED JITTER

BoundedWORST-CASE TIMING

What it does

Seeker fusion, state estimation, proportional navigation and autopilot are implemented in programmable logic, sized for a low-cost interceptor.

Worst-case timing is a property of the design, so the loop holds its deadline on every cycle rather than on average.

Worst-case timing for each stage is verified in hardware-in-the-loop test before anything flies.

Where it runs: A low-power adaptive module, with headroom for larger sensor suites.

Evidence

5 kHz

Guidance loop, zero measured jitter measured

A finalist in U.S. Army xTech|Apex Intercept, Topic 4, Fire Control and Flight Guidance. One of seven Topic 4 finalists, with a $25,000 finalist award.

U.S. Army xTech|Apex Intercept finals

Read the guidance core case study Read about the competition →

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