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.

The Aerospace & Defense Team's Business Service Providers (BSP) Directory is designed to help U.S. aerospace & defense companies identify professional service providers to assist them in the assessment, completion, and/or financing of an export transaction.

Revolutionary DFOG Technology Boreas takes Fibre Optic Gyroscope (FOG) technology into the next generation with new, patent-pending Digital FOG (DFOG) technology, developed over 25 years with 2 research institutions. This revolutionary DFOG technology combines a specially designed closed-loop optical coil with advanced spread spectrum digital modulation techniques that have never been used in a FOG before. The resulting DFOG offers dramatically improved accuracy, stability, and reliability with significantly reduced size, weight, power, and cost.

It is commonly used in industrial and other devices to generate triggers ranging from one to several thousand FPS, ensuring precise timing synchronization with various devices. Periodic Mode: Continuously generates trigger signals after configuration. Burst Mode: Generates a single trigger signal upon receiving the best command via serial communication. *** Product Expansion and Usage ***  Four Operating Modes  Periodic mode: Generates a single-cycle signal based on the configured frequency and duty ratio.  Burst mode: Generates a single-cycle signal synchronized with a software trigger.  External trigger mode: Generates a single-cycle signal synchronized with an external trigger.  External trigger bypass mode: Distributes signals triggered externally.  Connect the trigger output signals from a Master Trigger Generator to a Slave Trigger Generator (as shown below).  By connecting one of the Master TG’s Trigger Outputs (1 to 16) to the Slave TG’s External Trigger Input: Outputs 1 to 15 of the Master TG remain unchanged. Outputs 16 to 31 of the Slave TG will mirror the Master TG’s Trigger Output. (Note: Each trigger signal passing through a TG experiences a delay of ten ns. However, since trigger outputs operate in the range of tens to thousands of Hz, users will not notice the delay).  Example with 17 TGen-16C units: Produces up to 256 Trigger Output Channels (16 × 16).

Type : Axial (6P) Size(L,W,H mm) : 330 × 283 × 310 Weight(kg) : 54 N. Speed(rpm) : 2500 N. Torque(Nm) : 385 N. Power(kW) : 100

Spacecraft are exposed to extreme conditions that can jeopardize signal transmission capabilities, making it impossible for repairs in space. Whether traveling millions of miles for exploration or enabling global connectivity, space programs need durable solutions with reduced size and weight they can trust to perform without failure. W. L. Gore & Associates answers the call with small, low-mass GORE® Spaceflight Microwave/RF Assemblies proven to maintain electrical and mechanical performance in the harshest environments, ensuring mission readiness and success.

The new TAC-450-320/340/360 inertial measurement unit (IMU) is a dependable, tactical-grade, non-ITAR inertial system that’s also affordable. It features EMCORE’s exclusive photonic integrated chip (PIC) technology for robust performance and survivability and offers inertial-grade MEMS accelerometers for outstanding FOG-based inertial performance as affordable as MEMS alternatives. The TAC-450-320/340/360 IMU is ideal for autonomous and unmanned commercial and defense applications, mobile mapping and surveying systems, targeting and pointing systems, and guidance and positioning. Highlights Compact and lightweight with high-performance Offered with 16g inertial-grade MEMS accelerometer Robust performance with high bandwidth 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-450-320/340/360 IMU provides the safe, accurate performance autonomous platforms demand. State-of-the-art Electronics EMCORE’s Dual Core DSP electronics with ARM processor require less power for extended product life and offer higher speed with integrated multi-channel processing. Low-loss optical circuits use less light for greater efficiency. Feature Options Developer’s Kit for Rapid Integration The FOG/IMU Developer’s Kit includes easy-to-use software that accelerates your IMU and FOG integration, development, and interface efforts.

The CAS-500(Compact Advanced Satellite), phase #1 project is the project in which KAI aims to develop a CAS500-1 by operating a joint design team with Korea Aerospace Research Institute(KARI) and to transfer the government’s satellite development technology to the industries. Then, KAI initiates the development of the CAS500-2 project and establish the industry-led development as well as mass-production infrastructure.