# Key Features - Map Generation and No-Drive Zone Setting in Airports > Airport map/sensor fusion-based localization function > Function for defining main movement and standby areas > No-drive zone setting - Optimal Path Autonomous Driving Function > Destination-based optimal path navigation > Speed limit settings by path and area > Real-time location monitoring > Obstacle detection and immediate response > Driving on diverse road surfaces within designated areas - Real-Time Bird Detection and Bird Position/Direction Prediction > Real-time bird detection > Support for approximate bird position/direction prediction based on object detection algorithms > Updating of approximate bird position/direction prediction based on flock detection - Effective Bird Deterrence Reflecting Bird Characteristics > Playback of diverse (randomized) acoustic patterns - Real-Time Communication with Operator and Manual Control Function > Monitoring console (PC) provides real-time bird detection status and history > Display of approximate bird position/direction predictions on a map > Real-time video data sharing > Remote manual control - Smart Charging Function > Automatic return and charging when mission is complete or battery is low

Robotic technology that combines IoT and autonomous driving technologies provides key solutions for future mobility manufacturing. Main Functions Innovative manufacturing system using Collaborative Robot and Autonomous Mobile Robot ptimize production processes and provide logistics flexibility Ensuring Optimal Production Process Using AI Application Site HMGICs : Flexible Production Cells (smart manufacturing) Targeted to supply to global manufacturing sites

The SDI170 IMU is designed for demanding, mission-critical, rugged environments and ideal for continuous use applications with no wear-out components, highly linear accelerometer performance and longer life compared to competing alternatives. It is constructed with EMCORE’s latest generation quartz gyros, quartz accelerometers, and high-speed signal processing to achieve outstanding precision performance. The solid-state quartz sensors and hermetically sealed IMU construction provide reliable MTBF and a 20-year operating and storage life. Continuous Built-in Test (BIT), configurable communications protocols, electromagnetic interference (EMI) protection and flexible input power compatibility make the SDI170 IMU easy to use in a wide range of higher-order integrated commercial and defense system applications.

Between Earth and space: stratosphere-compatible, solar-powered high-altitude aircraft, known as HAPs (High Altitude Platforms), offer a sustainable alternative to satellites for Earth observation and communication. They are reusable, cost-effective and flexible in use. The DLR joint project HAP-alpha is developing such a technology demonstrator and is endeavoring to establish a complete system capable of permanent operation. The aim is for DLR to build up comprehensive expertise for the development of high-performance, high-flying solar aircraft and to play an active role in shaping the legal framework. In summer 2025, the HAP-alpha successfully passed a ground vibration test.

Saab's Electronic Warfare (EW) Countermeasure Dispensing Systems (CMDS) for airborne platforms provides self-protection in sophisticated, diverse and dense threat environments for your mission success and safe returns.

Large Area Display Head Unit is included in avionics equipments used in the cockpit of an aircraft. Its wide screen vision development implements Full Glass Cockpit in aircraft. It also provides processing with more efficient yet less complicated circumstance with maximum 4 external input video signals Options that can be provided are - 20"x8" LCD Glass, LCD Module and Entire LAD system unit

The AB-M1300 is a 1.3 ton-class eVTOL AAM. With a wingspan of 10 meters, the AB- M1300 is a crewed–uncrewed hybrid aircraft aiming for commercialization in 2028. Falling under the Light Sport Aircraft (LSA) certification category, it can carry up to two occupants, reach a maximum speed of 400 km/h, operate for two hour of flight time, has a maximum take-off weight (MTOW) of 1.3 tons, and a payload capacity of 250 kg. The AB-M1300 is designed for a variety of missions, including mid-mile logistics, personal leisure use, and pilot training.

The SC-HPCRTM is a Rear Transition Module (RTM) designed to extend the I/O functionality of the HPC2812 high-performance computing board. It can be mounted on the rear side of the VPX backplane to enhance system connectivity and I/O flexibility. Since the HPC2812 board consists of two computing nodes, the SC-HPCRTM provides dedicated interfaces for each node, including Ethernet, USB, MMCX, and Mini-HDMI ports, ensuring optimal data communication and display output performance in mission-critical embedded systems.