SmartPathTM FAA Certification
<P>SmartPathTM FAA Certification</P><P>**** Hidden Message *****</P> Dave Jensen, John Howard<BR>Honeywell, Precision Landing Systems<BR>29-30 Oct 2009<BR>CAAC New Technology Seminar - GNSS<BR>SmartPathTM FAA Certification<BR>􀃆 Honeywell.com<BR>SmartPathTM FAA Certification<BR>• SmartPath Certification Phases<BR>每 System Design Approval<BR>每 Facility Approval<BR>每 Operation Approval<BR>• FAA System Design Approval (SDA)<BR>每 SDA Life Cycle<BR>每 Aspects of SDA<BR>每 FAA/Honeywell SDA Effort<BR>• FAA Facility Approval<BR>每 Aspects of Facility Approval<BR>每 Facility Approval Activities<BR>Dave Jensen/John Howard<BR>2<BR>CAAC New Technology Seminar 每 GBAS 29-30 October 2009<BR>􀃆 Honeywell.com<BR>GBAS FAA Certification Phases<BR>• System Design Approval (SDA) 每 Manufacturer<BR>每 Ground station system design meets requirements<BR>每 Developed to appropriate design assurance levels<BR>每 Accuracy, integrity, availability requirements satisfied<BR>• Facility Approval 每 Owner/ANSP/Airport<BR>每 Ground station installed properly, safely<BR>每 Signal-in-space, coverage volume verified<BR>每 Maintenance technicians trained, certified<BR>每 Control tower personnel trained<BR>• Operational Approval 每 Operator/Airline<BR>每 Aircraft equipped<BR>每 Pilot crews trained<BR>每 Approach plates/procedures developed<BR>Dave Jensen/John Howard<BR>3<BR>CAAC New Technology Seminar 每 GBAS 29-30 October 2009<BR>􀃆 Honeywell.com<BR>FAA SDA Certification Life Cycle<BR>Systems & FHA Requirements, Architecture Phase<BR>Planning Documents & Subsystem Requirements Phase<BR>High Level Requirements Phase Year 1<BR>6-Mar-07<BR>MDT/ATSU<BR>3-May-06<BR>Honeywell GBAS<BR>18-Apr-07<BR>GPS<BR>4-Oct-06<BR>Phase Gate III<BR>27-Jan-07<BR>Phase Gate IV<BR>20-Apr-07<BR>GPS<BR>5-Mar-07<BR>RPDP HW<BR>30-Mar-07<BR>DCP SW<BR>25-Jul-06<BR>FAA/HI<BR>8-Feb-07<BR>DCP SW/HW<BR>15-Dec-06<BR>GPS SW/HW<BR>High Level Requirements Phase<BR>Proj Kickoff SDA Kickoff (PDR) FAA SOI 1 (CDR) FAA SOI 1 Dsn Rvw CDR Arch Rvw FAA SOI 2A CDR<BR>Development, Design and Low Level Requirements Phase<BR>Year 2 Verification Phase<BR>11-Mar-08<BR>RPDP<BR>5-Feb-08<BR>Phase 24-Sep-07<BR>31-Mar-08<BR>DCP 31-Aug-07<BR>DCP 18-Oct-07<BR>VDB<BR>17-Dec-07<BR>GPS<BR>4-Sep-07<BR>HI 13-Mar-08<BR>DCP 26-Sep-07<BR>FAA<BR>8-May-07<BR>DCP HW/SW<BR>Verification Phase<BR>FAA SOI 1/2<BR>DCP SW<BR>Gate V<BR>FAA SOI 2B<BR>HW<BR>FAA SOI 2<BR>HW<BR>FAA SOI 2B<BR>FAA SOI 1-4<BR>FAA SOI 2B<BR>Audit<BR>Telerad VDB<BR>SW<BR>FAA SOI 3A<BR>RTOS SOI 1/2<BR>-<BR>FAA SOI 2A<BR>FAA Audit Review Honeywell Design Activity<BR>Year 3 Results Review Phase Closeout Phase<BR>1-Dec-08<BR>GPS SW<BR>26-Jan-09<BR>DCP SW<BR>28-May-08<BR>GPS SW<BR>15-Dec-08<BR>GPS SW<BR>4-Dec-08<BR>TRR<BR>10-Nov-08<BR>Safety<BR>17-Sep-08<BR>DCP SW<BR>9-May-08<BR>FAA System<BR>20-Oct-08<BR>GPS SW<BR>26-Jul-09<BR>14-day<BR>5-Sep-08<BR>RTOS SW<BR>17-Mar-09<BR>FAA CIB<BR>25-Jan-09<BR>Formal V&V<BR>4-Sep-09<BR>FAA SDA<BR>Dave Jensen/John Howard<BR>4<BR>CAAC New Technology Seminar 每 GBAS 29-30 October 2009<BR>Verf. ReviewF A A SOI 3A FAA SOI 3/4F AA SOI 3B FAA SOI 3BF AA Rvw FAA SOI 4 FAA SOI 3C complete FAA SOI 4 Validation Stability Test Approval<BR>􀃆 Honeywell.com<BR>FAA SDA Certification Life Cycle<BR>• System Design (Year 1)<BR>每 Functional Hazard Assessment (FHA)<BR>每 System/Subsystem Design, Architecture and Requirements<BR>每 Preliminary System Safety Assessment (PSSA)<BR>每 Hardware/Software Planning Documents<BR>每 Design and Development of High Level Requirements (HLR)<BR>每 Preliminary Design Review (PDR)<BR>• Hardware/Software Development (Year 1-2)<BR>每 Design and Development of Low Level Requirements (LLR)<BR>每 Hardware and Software Implementation<BR>每 Hardware/Software Integration<BR>每 Critical Design Review (CDR)<BR>• Verification (Years 2-3)<BR>每 Development of Test Cases and Test Procedures<BR>每 Formal Run of Test Procedures<BR>每 Verification Results Review (VRR)<BR>• Formal SDA Submittal (Year 3)<BR>Dave Jensen/John Howard<BR>5<BR>CAAC New Technology Seminar 每 GBAS 29-30 October 2009<BR>􀃆 Honeywell.com<BR>SDA Hardware/Software Items<BR>SDA Item Subsystem<BR>• Differential Corrections Processor (Level 2)<BR>• Real-Time Operating System (Level 2)<BR>• GPS Receiver ( Level 2)<BR>Software<BR>Design Assurance<BR>(RTCA/DO 278 DO 178B)<BR>)<BR>• Ethernet Switch (Level 5)<BR>• VDB Receiver (Level 5)<BR>• VDB Transmitter (Level 5)<BR>DO-& DO-• Environmental Concentrator (Level 5)<BR>• Data Recorder (Level 6)<BR>• Maintenance Data Terminal (Level 6)<BR>• Air Traffic Status Unit (Level 6)<BR>Hardware<BR>Design Assurance<BR>• Differential Correction Processor (Level B)<BR>• GPS Receiver (Level B)<BR>g • Ethernet Switch (Level D)<BR>(RTCA/DO-254)<BR>• Data Recorder (Level E)<BR>• Maintenance Data Terminal (Level E)<BR>• Air Traffic Status Unit (Level E)<BR>Dave Jensen/John Howard<BR>6<BR>CAAC New Technology Seminar 每 GBAS 29-30 October 2009<BR>􀃆 Honeywell.com<BR>Software Development Process<BR>• Honeywell*s Design Assurance Level 2 Software Life Cycle<BR>Requirements<BR>Review (HLR)<BR>5.4.1.2.1<BR>Design Review<BR>(Arch & LLR)<BR>5.4.1.2.2<BR>Integration<BR>Review<BR>5.4.1.2.4<BR>A B C<BR>Code<BR>Review<BR>5.4.1.2.3<BR>• Requirement<BR>Reviews<BR>• Design Software<BR>Requirements<BR>(HLR)<BR>5 3 1<BR>Software<BR>Design<BR>(Arch & LLR)<BR>5 3 2<BR>Software<BR>Code<BR>5.3.3<BR>Integration<BR>Start 5.3.4 F G<BR>Reviews<BR>• Code Reviews<BR>• Integration<BR>5.3.1 5.3.2 Reviews<BR>Test Case<BR>Definition<BR>(HLR)<BR>Test Procedure<BR>Definition<BR>(HLR)<BR>Software<BR>Testing<BR>5 4 1 1 5<BR>Test Case<BR>Definition<BR>(LLR)<BR>Test Procedure<BR>Definition<BR>(LLR)<BR>F G C D E<BR>• Verification<BR>Independence<BR>• Test Cases<BR>Finish<BR>5.4.1.1.1<BR>Test Case<BR>Review (HLR)<BR>5.4.1.1.2<BR>Test Procedure<BR>Review (HLR)<BR>5.4.1.1.5<BR>Testing<BR>Review<BR>5.4.1.1.3<BR>Test Case<BR>Review (LLR)<BR>5.4.1.1.4<BR>Test Procedure<BR>Review (LLR)<BR>A B • Test Procedures<BR>• Configuration<BR>Management<BR>5.4.1.2.5 5.4.1.2.6 5.4.1.2.7 5.4.1.2.8 5.4.1.2.9<BR>D E<BR>Software Configuration Management 5.4.2<BR>Dave Jensen/John Howard<BR>7<BR>CAAC New Technology Seminar 每 GBAS 29-30 October 2009<BR>Software Quality Assurance 5.4.3<BR>􀃆 Honeywell.com<BR>SDA Systems/Safety/Verification/Training<BR>SDA Item Evaluation<BR>System Engineering<BR>• Requirements, Verification & Validation, Traceability,<BR>Design Reviews, Requirement Management, Change<BR>Management, Personnel Safety , Human Factors,<BR>(SAE/ARP-4754)<BR>g y<BR>Security, Reliability, Interface Control Documents,<BR>System Architecture, Quality Assurance<BR>• 14 System Safety Assessment<BR>(SAE/ARP-4754 & ARP-4761)<BR>GPS Integrity Monitor Algorithms<BR>• FAA LAAS Integrity Panel (LIP) - FAA and Key<BR>Technical Advisors approval of Safety Compliance<BR>and Safety Assessment<BR>System Verification<BR>(FAA-E-AJW44-2937A)<BR>• Demonstrate compliance with minimum performance<BR>requirements for non-Fed LAAS Ground Facility<BR>Commercial Instruction Book • Installation Configuration Operation Maintenance<BR>(FAA-D-2494)<BR>Installation, Configuration, Operation, Maintenance,<BR>Procedures, Troubleshooting, Parts Lists<BR>Training Program • Classroom, OJT Criteria, Examination, Certification<BR>Dave Jensen/John Howard<BR>8<BR>CAAC New Technology Seminar 每 GBAS 29-30 October 2009<BR>􀃆 Honeywell.com<BR>Total GBAS SDA Effort<BR>• 3 Years of Design, Development, and Verification<BR>• Over 230 Documents Submitted for Review<BR>• 23 Formal FAA Audits and Reviews<BR>• 10 Formal Internal Design Reviews<BR>• Over 2500 Hardware and Software Requirements<BR>每 Representing 21 subsystems<BR>每 Peer-reviewed, change controlled<BR>• Over 1500 GPS Corrections and Monitor Requirements<BR>每 Representing 14 integrity monitors<BR>• Over 2000 Test Cases<BR>每 To fully verify 4000+ requirements<BR>• Over 1200 Test Procedures<BR>每 To implement 2000+ test cases<BR>Peer Dave Jensen/John Howard<BR>9<BR>CAAC New Technology Seminar 每 GBAS 29-30 October 2009<BR>每 Peer-reviewed and formally run<BR>􀃆 Honeywell.com<BR>Aspects of Facility Approval (FAA)<BR>• Operational Concept<BR>• Technical Performance<BR>• Physical Integration<BR>• Functional Integration<BR>• Human Integration<BR>• System Security<BR>• In-Service Support<BR>• Test and Evaluation<BR>• Implementation and Transition<BR>• Quality Assurance<BR>• Configuration Management<BR>• In-Service Management<BR>• Safety Plan<BR>Dave Jensen/John Howard<BR>10<BR>CAAC New Technology Seminar 每 GBAS 29-30 October 2009<BR>y<BR>􀃆 Honeywell.com<BR>Facility Approval Activities<BR>• Flight Inspection<BR>每 Verify approaches<BR>每 Verify signal strength, coverage volume<BR>• FCC License<BR>每 Assigns broadcast frequency, power, time slots<BR>• Verify Installation<BR>每 Verify accuracy, availability, stability<BR>每 Complete SmartPath acceptance checklist(s)<BR>• Operation & Maintenance<BR>每 Document maintenance procedures<BR>每 Configure remote monitoring (read-only)<BR>• Spare Parts & Support Equipment<BR>• Training & Certification<BR>每 Maintainers, operators<BR>每 Control tower personnel<BR>Dave Jensen/John Howard<BR>11<BR>CAAC New Technology Seminar 每 GBAS 29-30 October 2009<BR>􀃆 Honeywell.com<BR>Recap<BR>• FAA/Honeywell System Design Approval (SDA) Included<BR>每 3 Year Development Effort<BR>每 HW/SW Design Assurance Rigor<BR>每 10 SW Design Assurance Items<BR>每 6 HW Design Assurance Items<BR>每 23 Formal FAA Audits & Reviews<BR>• FAA Facility Approval Includes<BR>每 Flight Inspection<BR>每 FCC License<BR>每 Verify Installation<BR>每 Personnel Training & Certification<BR>每 Spare Parts & Equipment<BR>•Questions?<BR>Dave Jensen/John Howard<BR>12<BR>CAAC New Technology Seminar 每 GBAS 29-30 October 2009 洷咡艘善FAA 勍褫佷繚
珜:
[1]