Common Open Reuse Environment (CORE) Cockpit
High Re-use, Lowest Risk, Affordable
• In partnership with the DoD, development, integration and test of the software and avionics solution addresses CNS/ATM Navigation-Safety compliance, Net Readiness, and legacy Avionics obsolescence.
• Previously integrated instantiations of the CORE cockpit enables a high-reuse CNS/ATM compliant solution.
• The CORE cockpit, when complemented with Lockheed Martin’s breadth of expertise, provides customers a complete offering from installation, training, transition, and organic support.
![CORE](/content/dam/lockheed-martin/rms/photo/avionics/C-130T_Cockpit%20_MOR201903019.jpg.pc-adaptive.full.medium.jpg)
Lockheed Martin provides the cockpit, integrated avionics and mission systems on the V-280 Valor for the U.S. Army’s Joint Multi Role (JMR) and Future Vertical Lift (FVL) programs and embraces a Modular Open System Approach (MOSA) by:
• Developing an integrated CORE digital glass cockpit and avionics system that utilizes the FACETM reference architecture.
• Providing the foundation of the software applications used on V-280, leveraging re-useable software and contributing back to the software library.
• Significantly reducing development costs, schedule, and risk, helping to address obsolescence impacts on current and future cockpit and avionics systems.
Flight-proven Fielded Cockpit
• The Lockheed Martin CORE Cockpit first flew in December 2017, which was Lockheed Martin’s first flight of a fully “app-based" cockpit and avionics system.
• The CORE open architecture design positions the V-280 to accept additional avionics equipment and mission system capabilities to meet the needs for the next generation rotary wing aircraft
![V-280](/content/dam/lockheed-martin/rms/photo/avionics/V-280.jpg.pc-adaptive.full.medium.jpg)
The Lockheed Martin Common Open Reuse Environment (CORE) cockpit represents the first fielded all “app-based” cockpit and avionics solution that was originally designed to be in alignment with the FACETM standard, providing customers with a truly open and scalable avionics solution to address evolving civil and tactical airspace requirements. Central to this scalable architecture is a unique Flight Management System (FMS) which fully integrates tactical and civil airspace functionality providing the flight crew with a single seamless flight plan which can interleave civil and tactical waypoints thereby enhancing mission effectiveness.
Full CNS/ATM Functionality
• LPV (Localizer Performance with Vertical Guidance) per AC 90-107
• RNP 0.3 & Baro-VNAV per DO-236B
• ADS-B per AC 20-165A, DO-260B
• WAAS GPS per TSO-C145c, TSO-C146c
• TAWS per TSO-C151b, FAA Notice 8110.64
• TCAS per DO-185B
• MFD per DO-257A, DO-185B
• Enhanced Mode S (EHS) per ICAO Annex 10
• ACARS/CPDLC per; ATN Baseline 2, ARINC-739 via VDL Mode 2 and Iridium SATCOM
Blended Tactical Functionality
• CARP per AFI 11-231
• Search and Rescue Patterns per Joint Pub 3-50 SAR Manual
• Refueling Patterns per ATP-56
• Anti-Jam SAASM GPS with M Code
• IFF Mode 5
• Self-contained Tactical Approaches
![C130](/content/dam/lockheed-martin/rms/photo/avionics/CORE_Images-1.jpg.pc-adaptive.full.medium.jpg)
![C130](/content/dam/lockheed-martin/rms/photo/avionics/CORE_Images-2.jpg.pc-adaptive.full.medium.jpg)
![v280](/content/dam/lockheed-martin/rms/photo/avionics/CORE_Images-3.jpg.pc-adaptive.full.medium.jpg)
![v280](/content/dam/lockheed-martin/rms/photo/avionics/CORE_Images-4.jpg.pc-adaptive.full.medium.jpg)
Common Product Library (CPL)
CPL Advantages:
• Increasing reuse and reliability
• Decreasing time to deployment and development risk
• Optionally configured to support security requirements
• Flexibility and scalability
• Easy upgrades and maintainability as technology advances
• Designed for ease of upgradability (COTS cards can easily be upgraded to the latest technology)
CPL SW Features:
• Designed in alignment with FACETM standard
• 180+ portable SW components
• 400,000 lines of reuse SW code
• Designed to meet DO-178B/C safety-of-flight requirements
![CORE](/content/dam/lockheed-martin/rms/photo/avionics/C130038_EDIT-01.jpg.pc-adaptive.full.medium.jpg)
Controls & Displays Features:
• True, hemispherical viewing cone in portrait or landscape orientation
• Configurable to operate from four to eight displays
• NVIS certified
• Dual Graphics/Processor Cards support flight/mission applications concurrently with Digital Map function
• Flexible Graphical User Interface
Integrated Software Applications:
• More than 180 ARINC-653 time/space partitioned portable software components designed in alignment with FACE™ standard
• These software components include the applicable data and software rights to allow third party integration of other FACE™ conformant software components
Portable Software Components consist of these three categories:
• Device Drivers: isolate unique interface requirements for each hardware subsystem enabling rapid subsystem reconfiguration
• Graphics Skins and Widgets: separates the look and feel of the graphics from the core graphic processing providing multiple display configuration option without affecting certification
• Functional Applications: breaks functional operational capabilities into their functional subcomponents providing rapid mission reconfiguration e.g. Flight Management System