The HG2802 is a higher operating range option within the HG2800 family of high-performance tactical grade IMUs that includes Honeywell’s next-generation micro-electro mechanical systems (MEMS) accelerometers in addition to closed-loop fiber optic gyros (FOGs), providing improved dynamic range and scale factor linearity performance. These IMUs are developed to affordably meet the needs of a broad range of guidance and control applications.
Its small-size, light-weight, high-bandwidth, low-noise, zero-maintenance configuration makes the HG2800 IMUs ideal for electro-optical (EO)/FLIR stabilization, camera/radar stabilization, pointing and positioning, mapping/inspection, autonomous underwater (AUV) and UAV navigation, odometer/DVL, and silent operation for acoustic-sensitive systems.
The HG2800 flexible power supply design simplifies system integration for a single +5V supply voltage or dual +15V, +5V supplies, while consuming less power than competing fiber optic gyro-based IMUs in the market.
As our first-ever Tactical FOG IMU, the HG2800 series fills an important void for commercial and government entities needing precision imaging, platform stabilization and low noise acoustically-sensitive navigation and stabilization solutions. The HG2800 is a dual-use non-ITAR restricted IMU designed specifically to meet both commercial/industrial and military needs.
Yes, we retrofit legacy systems (e.g., GE Frame 5, Siemens V94.2) with modern digital controllers, typically completing hardware integration within 4-8 weeks. Software migration requires additional validation time.
We recommend annual performance testing under ISO 3977-2 standards. Critical applications (e.g., offshore platforms) may require semi-annual tests with emissions compliance checks.
All rad-hard devices (e.g., FPGA, ADC) are QML Class V certified under MIL-PRF-38535 and tested to MIL-STD-883 Method 1019 for SEU tolerance. Full qualification reports are available upon request.
Our ASICs and power management ICs operate across -55°C to +175°C ambient temperatures, with derating curves provided in military temperature range (MTR) datasheets.
Our PMA parts (e.g., actuators, sensors) hold FAA/EASA Form 1 certification and match OEM form/fit/function. Installation requires SB/MB documentation per FAA AC 23.1529.
All NAS/MS fasteners include full DNA traceability: melt source (AMS 2301), heat/lot numbers, and AS9100-compliant MTRs with ultrasonic test reports.
AOG orders ship within 4 hours for stocked items (FAA-PMA, EASA Part 21G). Non-stock critical parts trigger priority manufacturing with 72-hour max turnaround.
Gas Turbine
Aircraft parts
