Ultra-High Accuracy MEMS Certus Evo features some of the highest accuracy MEMS accelerometers and gyroscopes currently available. Certus Evo’s inertial performance exceeds some FOG IMUs and is up to 100x smaller and 10x cheaper. Certus Evo is put through Advanced Navigation’s intensive calibration process to provide consistently accurate data over an extended temperature range of -40°C to 85°C. AI-Based Algorithm Certus Evo features Advanced Navigation’s revolutionary AI neural network sensor fusion algorithm. It was designed for control applications and has a high level of health monitoring and instability prevention to ensure stable and reliable data. Dual Antenna RTK GNSS Certus Evo contains a dual frequency RTK GNSS receiver that provides up to 1 cm accuracy positioning and supports all of the current and future satellite navigation systems, including GPS, GLONASS, GALILEO, BeiDou and QZSS. Dual antenna heading provides high accuracy heading that is not impacted by magnetic interference and has no motion requirements. Time Synchronization Certus Evo contains a GNSS disciplined oscillator that can act as the primary time source within a distributed time system, enabling access to ultra-accurate system time using PTP or NTP network time sync. Certus also has a high-accuracy 1PPS and frequency output. Multi Protocol Support Certus Evo features multiple interfaces including Ethernet, CAN, RS232, RS422 and GPIOs. Certus supports all the industry standard protocols including NMEA 0183, NMEA 2000, TSS, PASHR, Simrad as well as a wide variety of proprietary protocols. It features a rich web UI and 256GB of internal logging.

A next-generation Advanced Air Mobility (AAM) aircraft currently under development, designed with a separable upper platform and lower mission module structure. The interchangeable lower modules can be configured for passenger transport, cargo delivery, or reconnaissance missions, offering exceptional operational flexibility across various applications. As a large-scale platform, it embodies the future of modular air mobility, enabling rapid mission conversion, efficient maintenance, and cost-effective operation for both urban and regional air mobility sectors.

We manufacture clamps, latches, hinges, fasteners, exit door handles etc.

Dynamic Load Carriage® system Dim. : 6.5" W PALS webbing for MOLLE attachment Patented Ballistic Vein® Composition Material : 500D Cordura® + ARAMID / PV® Size : SMALL 26" - 30" MEDIUM 29" - 33" LARGE 32" - 36" XLARGE 36" - 40" Colors: MC (MultiCam) BMC (Black MultiCam) BK (Black) RG (Ranger Green) CYT (Coyote Brown)

This solution follows a three-step process of input, processing, and output, utilizing imagery, DEM, AT, and spatial data to refine 3D models. The editing-based texturing function allows users to correct shape errors, occlusions, and distortions, while the automated texturing ensures consistency and accuracy through advanced geometric matching. Final outputs are stored in standard formats for broad practical applications.

FOBEX 38999 MIL-DTL-38999 An optical connector which is applied to beam expanding optical signal transmission technology into a connector designed according to military standards. It can be used in a variety of adverse conditions such as extreme temperature, vibration, shock, humidity, and dust. It has little impact from outdoor contamination and is easy to maintain, making it easy to use tactically. FOBEX 83526 Ensures stable and reliable data transmission in extreme environments. Designed with a hermaphrodite type for easy connection and disconnection over 3,000 times, the extended beam technology minimizes loss caused by dust or contaminants from outdoors. FOBEX-P Fiber optic ferrules with expandable beam technology, designed to replace 1.6mm military fiber optic ferrules for tactical applications

[LEO GNSS-R] Satellite : LEO RF Characteristics : GPS L1/L5, Galileo E1/E5a(option) Accuracy : Position ≤ 10m(3DRMS), Velocity : ≤ 1m/s Raw Data Accuracy : Pseudo-Range : 1m(RMS) Carrier-Phase : 10mm(RMS) Data Output Rate : 1Hz 1PPS Accuracy : Sync to GPS Time Data < 1us (1PPS Accuracy < 1.5us) TTFF : Cold Start ≤ 20min / Warm Start ≤ 10min Dara Interface : MIL-STD-1553B, RS-422(Data Interface) [GEO GNSS-R] Satellite : GEO RF Characteristics : GPS L1/L2C/L5, Galileo E1 Accuracy : Position :: ≤ 30m(3DRMS), Velocity : ≤ 1m/s Raw Data Accuracy : Pseudo-Range : 1m(RMS) Carrier-Phase : 10mm(RMS) Data Output Rate : 1Hz 1PPS Accuracy : 2us(RMS)/Sync to GPS Time Data TTFF : Cold Start ≤ 45min / Warm Start ≤ 20min Dara Interface : MIL-STD-1553B EEE Parts : ITAR Free Parts

Heat engine that converts combustion energy into mechanical energy. It consists of a compressor, combustion chamber, and turbine, and is widely used in aircraft propulsion.