Collects data from various sensors within the aircraft system, converts it into the required format, and transmits it to the mission computer or flight control computer. Converts control commands received from the mission computer or flight control computer and relays them to sensors and other peripheral devices. Supports system control functions, monitors the status of key systems, and provides feedback. Achieves 70% cost competitiveness compared to equivalent-performance products. - x2 MIL-STD-1553B - x2 UART (RS-422/485) - x24 Analog input interfaces - x8 Analog output interfaces - x64 Discrete input interfaces - x40 Discrete output interfaces - Size : 270 x 270 x 62.2mm - Weight : 2.5Kg - Power : MIL-STD-704F (28VDC, 10W) - Environment : MIL-STD-810G - EMI/EMC : MIL-STD-461G

The TAC-450 FOG offers exceptional performance in bias stability, scale factor, and angle random walk, and is available in nine configurations to solve the most challenging design projects. The TAC-450 FOG is ideal for air, land, or maritime stabilization and pointing applications. Due to its versatility, and accurate, reliable output, it can also be utilized in navigation, guidance, and control systems. Highlights Designed for maximum ease of integration with housed or unhoused (for OEM configurations) options Available in nine configurations to solve the most challenging design projects Exceptional performance in bias stability, scale factor, and angle random walk 1-, 2-, or 3-axis configuration, each employing the world’s smallest precision FOG Technology Details Photonic Integrated Chip Technology EMCORE’s photonic integrated chip (PIC) technology* reimagines FOG technology by replacing individual fiber components with an innovative integrated planar optic chip. This results in a FOG with PIC Inside™ that’s reliable and robust. With three of these integrated photonic gyros at its core, the TAC-450-360 IMU provides the safe, accurate performance autonomous platforms demand.

PELICAN-D JT is a MWIR detector for missile applications. The FPA is InSb based, having digital Readout Integrated Circuit (ROIC) in a format of 640 x 512 with 15μm pitch. Pelican-D JT has a unique structure of Dewar which enables very fast cool down time and hence quick mission readiness using Joule-Thomson (JT) cooler. Due to the low heat load on the focal plane, the detector achieves long mission duration. The Detector can be supplied with a proximity board which provides Camera Link interface to the customer system. This highly simplifies the integration of the detector to the system.

This is the UAV launchers capable of launching the fixed-wing UAVs even on mountainous terrain, field, ships without sufficient runways to take off. It is designed to be the most powerful and easy to operate to take off the fixed-wing type UAVs of various specifications(Take-off weight, Take-off speed, and allowable G-force) into the air. It provides an interface that standardizes the shuttle for any type of unmanned aviation vehicle, and is easy to mount and to avoid take-off interference. A specially designed and manufactured hydraulic actuator is used to fully cope with the take-off weight of the aircraft, and a proprietary accumulator to allow a wide range of launch speed control. And multiple pulleys are equipped to ensure acceleration performance.

Integrated logistics support division, a Vendor Item Tool Manager, Consumables & Special Cutting Tools, Fixed and Rotary Wing String Lighting.

The fully redundant DA 30-HT-D has been developed for applications with the highest reliability demands. The redundant – two channel – design of the actuator allows continuous operation even if one of the two channels has failed. All major components such as the electric motors, control and communication electronics, and power supply are available twice (redundant). The position sensor features a three channel design (for 2 out of 3 voting). Additionally, there are several sensors integrated to provide diagnostic information such as current consumption, supply voltage levels and temperature readings. All major components of the actuator are continuously diagnosed by the microcontrollers of the actuator and its health status can be read via the redundant RS485.

The AB-U60 is a 60kg-class vectored-thrust eVTOL aircraft designed for surveillance and emergency logistics. Developed in response to the growing global demand for disaster response and urgent logistics solutions, the AB-U60 can be adapted for a variety of industries, including wildfire monitoring, anti-drone operations, and ship resupply. It combines an advanced fanjet electric propulsion system with a hybrid energy source to achieve high-speed flight and extended endurance. Airbility’s AB-U60 provides key advantages over competitors, offering high-speed flight of up to 200 km/h and vertical takeoff and landing capabilities for operations in confined spaces. Its low-noise fanjet propulsion system makes it suitable for both urban and suburban missions. The aircraft is also equipped with real-time data analysis and AI-based autonomous flight control systems. These features enable more efficient and safer operations.

Original compact design and long-term production know-how. System reliability and overall competitiveness.