Hexagon US Federal 725M Integrated System

The US Air Force is conducting market research to determine the existence of potential sources to provide high-precision, ruggedized Global Navigation Satellite System (GNSS) and Inertial Navigation System (INS) receiver hardware. The purpose of this hardware is to deliver highly accurate, reliable, and continuous Position, Navigation, and Timing (PNT) data within contested electromagnetic environments to support intelligence, surveillance, and reconnaissance (ISR), tactical vehicle navigation, precision targeting, and benchmark-quality testing/operator training. The key technical requirements for the system include: • Data Output Rates: Must support a sustained 20 Hz GNSS data output rate and a 100 Hz raw IMU data output rate • Sensor Fusion & Integration: Must support tightly coupled GNSS/INS integration utilizing tactical-grade Micro-Electro-Mechanical Systems (MEMS) Inertial Measurement Units (IMUs) • Constellation & Signal Tracking: Simultaneous tracking of multi-constellations and signals including GPS, GLONASS, Galileo, BeiDou, QZSS, NavIC L5, and SBAS • Interference & Spoofing Resilience: Embedded, advanced software/firmware-level interference mitigation and active spoofing detection • Secure Military GPS Integration: Must utilize a modified-commercial architecture capable of integrating with the L3Harris M-Code Increment 1, Type 2 receiver architecture • Hardware Form Factors & Interoperability: Systems must be compatible or form-fit-function equivalent with existing test-bench environments Interested parties are invited to submit a Capability Statement detailing their company information, technical capability, interoperability, and authorized channels.