A Customer Required a Real-Rime Hybrid Hardware-In-the-Loop System Controller.
The System Must Support Full HIL Configurations With Physical EGI Capabilty, Reduced HIL With Simulated
EGI Navigation Simulation and Flight Test Modes.
Provide Multiple Methods of Real-Rime Trajectory Generation: 6-DOF, Ethernet, File(Precise 3-DOF, 6-DOF High Rate, End-User Methods)
200Hz Trajectory Updates to RF generators. 600Hz Updates to IMU Injection
F15 / F16 / C130 EGI Control / Interfaces and Data Translation
Scenario Generation, Scripting, Plots, Logs Displays, Data Reduction
Visualization / Situational Awareness
Navigaton Data Manager / Server: Various Platfrom Navigator Formats over MIL-STD-1553, RS422, Ethernet
Precise Time Synchronization for 6-DOF / RF Generator(s) Updates, Synchronous I/O, Time Stamping of All Data
Trajectory Models: Land, Sea, Airborne, Space in Various Navigation Frames: ECI, ECEF, WGS...
Link-16 Message Simulation
Compensation for Hardware Update Rates
Synergy of three efforts: (1) SBIR funded Real-Time Network Centric Warfare Evaulation Test System (RTNETS),
(2) SBIR Geolocation Simulation Environment Toolset (GEOSET),
(3) IDIQ CORE Software Development.
The agressive developmental time-line and broad scope required symbotic development via the three programs. As a result,
the CORE concept of common reueable libraries of real-time architecture, I/O methods, communications, devices etc was established.
Each USAF customer received the applicable updates and capabilties to their common CORE software.
Limited to Authorized Users. Contact NST for Additional Information Associated With Complex Hybrid HIL and How CORE Can Advance Your Development Schedule.
Note: Things Change Rapidly! Specifications, Capabilities, Features and Availability Subject to Change Without Notice and May Be Restricted to Certain Users.