For Ground, Sea, Air, and Space Application

The Pseudo-GNSS system is designed with tightly integrated firmware and hardware. The firmware generates PRN signals based on GNSS orbital data, modulates them to resemble real GNSS signals, and ensures time synchronization in a Master-Slave structure. A user-friendly GUI software enables easy device control. The hardware consists of a power unit, signal transmission unit, and communication unit. The power unit ensures stable supply through low-noise design, while the transmission unit radiates GNSS-like signals indoors. The communication unit supports Wi-Fi and wired connections for synchronization and control across multiple devices, with compatibility for smartphones and tablets to display positioning results.

GAIN CRITICAL CLARITY WITH SATELLITE TASKING Task ICEYE SAR satellites to access groundbreaking data on any location on Earth – day or night and in any weather. The process is simple and images are usually delivered within 24 to 48 hours of your initial request. ORDERING SAR DATA – MADE SIMPLE We believe access to reliable and timely SAR Earth observation data should be available to all, so we provide access options designed to meet your specific mission needs and collection timeframes. The process begins with defining your area of interest, revisit frequency and other parameters. The first images are usually acquired, downlinked, decoded and processed within 24 hours of the initial request and delivered within 8 hours after that.

RFcore has been innovating MMIC solutions for phased array system pursuing more ease of use, higher performance, higher level of integration as well as lower cost. We believe that the most suitable way is exploiting properties of God gifted semiconductor Silicon and GaN. We aim at integrating all components of TRM for active phased array on single die and even multi-channel TRM too.

To guarantee maximum safety and reliability, our DA 30 features a brushless motor and a contactless wear-free position sensor. This means maximum service life with the greatest‐possible power delivery and its design prevents electromagnetic emissions (EMI) caused by brush sparking. The housing made of saltwater‐resistant aluminum is HART‐coat treated, meets the IP‐67 standard for water and dust sealing and provides an integrated Sub‐D connector (MIL spec. circular connector or cable gland on request). Brackets integrated in the housing for horizontal and vertical assembly. 8‐fold, ball‐bearing supported, steel gear train, drive shaft with ANSI multi‐tooth. The DA 30 series can be equipped with a standard PWM input (Pulse Width Modulation) that has two different interfaces: a differential, galvanic isolated interface (Opto‐Coupler) and a single‐ended interface with CMOS levels that is also used to program the servo parameters. It includes analog position feedback to detect the drive shaft position. A differential RS‐422 PWM interface can be chosen instead of the opto‐coupled interface. The DA 30 with digital serial command interface (RS‐485) receives its commands via a CRC secured protocol. It can return not only the shaft position in digital format, but also several diagnostic data such as the level of the supply voltage, current consumption and the temperature of the motor and electronics in digital form (optionally also the humidity within the actuator case). These kind of diagnostic capabilities help to determine the health state of the actuators before, during and after deployment.

Providing comprehensive training in the defense/aviation field and comprehensive logistics support system solution [CBT/LCMS] Analysis and application of ISD development methodology, 2D/3D modeling and animation production, application of OSMU (One Source Multi Use), application of SCORM standard for reuse and interoperability, development of CAI authoring tool [AR/VR] More than 100 multiple connections, omnidirectional interaction, high-precision content and processing engine, multi-platform support [TIMS] Pilot/mechanic training management, e-government framework, application of training history/grade/learning evaluation management function, development of other system linkage functions (C4I, DELLIS-F) [Training Equipment] Aerodynamic model development and HOST SW development, in-house development of image generator and data base production, aircraft aviation/navigation/system simulation and system design/integration and testing [Avionics & ETS] Embedded LRU and driver development, mission training, virtual radar/EO development, aircraft interworking and test evaluation [Comprehensive Logistics Support] Possessing ILS development capability, development of ground support equipment, mobile dehumidifier, aircraft MRO [Motion/Control Reaction Force/Vibration System] Provides motion, control reaction force, and vibration system for simulator system integration

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.

The vast range of ABC products allows us to meet the greatt majority of customer requests. Many products exist in our catalog and can be declined either through AMM or CMM, or through aircraft, or through more universal functions. Thus we propose test means associated with capabilities (universal benches) or associated with particular components (CMM) ...