Legacy C-130 Cockpit Upgrade Solutions John Kiernan Lockheed Martin
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Legacy C-130 Cockpit Upgrade Solutions John Kiernan Lockheed Martin
Legacy C-130 Cockpit Upgrade Solutions John Kiernan Lockheed Martin Mission Systems and Training (607-751-4375, [email protected]) INFORMATION CONTAINED IN THIS BRIEFING IS FOR REFERENCE PURPOSES ONLY AND DOES NOT NECESSARILY REFLECT THE LATEST AIRCRAFT MODEL(S) OR CONFIGURATION(S). THIS PRESENTATION IS FOR INFORMATION ONLY. NO US GOVERNMENT COMMITMENT TO SELL, LOAN, LEASE, CO-DEVELOP OR CO-PRODUCE DEFENSE ARTICLES OR SERVICES IS IMPLIED OR INTENDED. Copyright 2013, Lockheed Martin Corporation. All rights reserved. C-130T AOU Program Overview PROGRAM: C-130T Avionics Obsolescence PICTURE OF PLATFORM GOES HERE Upgrade Program CUSTOMER: PMA-207 PROGRAM OBJECTIVE: Provide an integrated cockpit solution (mix of GFE/CFE) to address DMS, CNS/ATM and Future Growth EMD Contract Scope: LM MST provides Cockpit “Kit” to NAVAIR • MST “Kit” SW Integrates 19 GFE subsystems w/ 20 LM provided WRAs • Develop full lab capability w/ Cockpit Mock-Up • Training Curriculum • 9 Kits (2 lab, 2 trainers, 3 Flt Tst AC, 2 LRIP) • Production options to follow Copyright 2013, Lockheed Martin Corporation. All rights reserved. LM C-130 Cockpit Features Designed for Retrofit Market: Small “foot print” - no Mission Computer, modular HW configuration •Qualified for severe environments, no “cocooning” required (MIL-STD-810G, 704A, 461F) Scalable to address multi-mission: Full CNS/ATM compliance for world wide airspace access : • RNP - 0.3 per DO-236 and Navy FRD • LPV (precision GPS) Approaches, WAAS/SAASM GPS • All ARINC-424 leg types for future growth • Supports both DAFIF and Jepp Nav Data concurrently • ADS-B, EHS Mode S, and Civil DL (ACARS/CPDLC) • Seamless Civil/Tactical flight plans Copyright 2013, Lockheed Martin Corporation. All rights reserved. •ARINC-653 SW partitioned and FACE SW provide maximum SW modularity •Display / CDU Formats designed for easy reconfiguration • Cockpit configuration is table driven •Customer can own “look/feel” and configuration of the cockpit •ARINC-739 CDU supports 3rd party integration NDI HW Baseline offers low risk solution: • All HW fully qualified, no HW development •Maximized reuse from existing C-130H and C-130J programs • SW is abstracted from HW to address DMS impacts Designed for portability: • Core of cockpit is being used for Helicopter and Tilt-Rotor Applications C-130 System Block Diagram RT BC BBC BBC DFDCP BBC Eng Inst DFDCP ADC (2x) TCAS/TAWS Wx Radar AFCS RT IFF ISS CCD CCD RT RT RT Gbit Ethernet Switch RT VOR/ILS (x2) Civil GPS (x2) RT DF Nav (2x) Data Recorder/ Bulk Storage RT FECDU/FMS RT CDU/FMS CDU/FMS BBC BC TRANSFER-BUS* BC Data Loader BBC BBC BBC FM-BUS RT C-406 ELT EGI (2x) MIL-STD-1553B Video RT RT RT DF SAR TACAN ARINC-429 Discrete Dedicated Ethernet VUHF 1 RT VUHF 2 RT VUHF 3 ICS RT RT HF 1 HF 2 Toughwriter IV Copyright 2013, Lockheed Martin Corporation. All rights reserved. CMU Civil VHF Civil SATCOM LM Value Proposition FACE = Future Airborne Capability Environment Portable SW Component OS & I/O Services Unrestricted Rights Defined Standards Processor Hardware Aircraft Systems Common Services Platform Serv Unrestricted Rights Defined Standards Transport Serv Avionic Systems PVI Benefits: • Designed for Full FACE™ conformance • Allows 3rd Party Integration • Portability of applications • Isolation of SW from HW reducing DMS impacts • First Avionics solution fully built on FACE architecture • No Proprietary Interfaces •ARINC-653 SW Partitions • ARINC-739 CDU • Customer Can own formats Real World Example <2 weeks • Portrait to Landscape display – same core SW/HW • Added Bezel control vice panels • All new formats • New CDU – same SW core different GUI QUESTIONS