The file's text, extracted by GovTribe without its formatting.
PREPARED BY
| CAGE CODE 2D605 |
| NUMBER |
| REV |
The Boeing Company
| APPROVALS |
| SPACE AND INTELLIGENCE SYSTEM |
| ENGINEERING |
CS-SW
Mark Kostelic
AUTHORITY
CS SEIT
Becky Gaede
08 Sept 2010
SUBJECT
| EFFECT ON: RELEASE TO FILES |
| CHANGE/RELEASE |
PSDR/NR
SOFTWARE REQUIREMENTS SPECIFICATION
FOR THE
POSITIONAL TRAINING EMULATOR
OF THE GLOBAL POSITIONING SYSTEM BLOCK IIF
CONTRACT NO. F04701-96-C-0025
ADPL SEQUENCE NO. 025-4
Prepared for:
U.S. AIR FORCE
HEADQUARTERS SPACE & MISSILE SYSTEMS CENTER
LOS ANGELES, CA 90009-2960
Prepared by:
BOEING
SPACE AND INTELLIGENCE SYSTEMS
2201 Seal Beach Blvd
Seal Beach, CA 90740
Distribution D: Distribution authorized to DOD and US DOD contractors only. (Reason: Administrative or Operational Use) (Date of Determination: 28 September 1995). Other requests for this document shall be referred to NAVSTAR Global Positioning System Joint Program Office (SMC/CZ).
WARNING: This document contains technical data whose export is restricted by the Arms Export Control Act (Title 22, U.S.C. 2571 et seq.) or Executive Order 12470. Violation of these export control laws is subject to severe criminal penalties. Dissemination of this document is controlled under DOD directive 5230.25 and AFI 61-204. Include this notice with any reproduced part of this document.
DESTRUCTION NOTICE: For classified documents, follow DOD 5220.22M, National Industrial Security Program Operating Manual. For unclassified limited documents, destroy by any method that will prevent disclosure of the contents or reconstruction of the document.
FORM 3935-G-1 REV 1-97 (Word 7.0)
Document Revision & Version History
| Revision for SRS-PTE-Phase 4 |
| Date |
| Event |
| New |
| 26 March 2009 |
| Initial Release |
| A |
| 9 June 2009 |
| Renumbering of Requirement IDs to Section 3.0 and Appendix A |
| B |
| 9 Sept 2009 |
| Updates for AEP V5.5 |
| C |
| 12 March 2010 |
| Action Item #PTE-002 from FCA/PCA. Change requirement from PTE SS-PTE-77E156 to PTE-77 in Table 2. |
Action Item PTE-018 from FCA/PCA. Added Missing IIF Training Capabilities for PTE-SRS-3290, PTE-SRS-3292,and PTE-SRS-3293.
| D |
| 19 July 2010 |
| Updates for V5.5.3 and PTE-KDW-033. |
| E |
| 08 Sept 2010 |
| Updates from PTE-KDW-034 which includes documentation inconsistencies between SOW and PTE-PA-011, PTE-VA-023, PTE-VA-010, PTE-PA-006, PTE-VA-007, PTE-VA-004, PTE-PA-013, |
Notices
The following terms are trademarks, registered trademarks, or service marks of other companies and organizations. Each term is the property of its respective owner.
| X Window System |
| Massachusetts Institute of Technology |
Table of Contents 11 Scope
11.1 Identification
11.2 System Overview
11.2.1 PTE Mission
21.2.2 PTE Software Overview
21.3 Document Overview
21.3.1 Document Requirements Terminology and Use
32 Referenced Documents
32.1 Government Documents
32.1.1 Specifications
32.1.2 Standards
32.1.3 Drawings
32.1.4 Other Publications
42.2 Non-government Documents
42.2.1 Reference Documents
42.2.2 Specifications
42.2.3 Standards
52.2.4 Drawings
52.2.5 Other Publications
63 Requirements
63.1 Required States and Modes.
63.2 Software System Requirements.
63.2.1 Hardware
63.2.2 PTE Capability Requirements
103.2.3 Crew Training.
103.2.4 Positional Training
103.2.5 Basic Operator (BOPR) Training
103.2.6 Advanced Training Capabilities (Advanced Operator Training).
113.2.7 PTE MCS External Interface Requirements.
113.3.1 Interface Identification and Diagrams.
113.3.2 Project Unique Identification of Interface.
113.3.3 PTE MCS System External Interface Requirements.
113.4 PTE Internal Interface Requirements.
113.5 PTE Internal Data Requirements.
113.6 Adaptation Requirements.
113.7 Safety Requirements.
123.8 Security and Privacy Requirements.
123.9 PTE Environment Requirements.
123.10 Computer Resource Requirements.
123.10.1 Computer Hardware Requirements.
123.10.2 Computer Hardware Resource Utilization Requirements.
123.10.3 Computer Software Requirements.
123.10.4 Communications Requirements.
123.11 Software Quality Factors.
123.12 Design and Implementation Constraints.
133.13 Personnel Related Requirements.
133.14 Training Related Requirements.
133.15 Logistics Related Requirements.
133.16 Other Requirements.
133.17 Packaging Requirements.
133.18 Precedence and Criticality of Requirements.
144 Qualification Provisions
144.1 Test Program
154.2 Verification Methods
154.2.1 Demonstration.
154.2.2 Test.
154.2.3 Analysis.
154.2.4 Inspection.
165 Requirements Traceability
176 Notes
176.1 Acronyms
196.2 Technical Glossary
List of Appendices
110 APPENDIX A: Requirements Traceability and Verification Cross Reference A-
120 APPENDIX B: Basic Operator (BOPR) Training Capabilities B-
130 APPENDIX C: Vehicle Advanced Training Capabilities C-
140 APPENDIX D: Payload Advanced Training Capabilities D-
150 APPENDIX E: Crew Advanced Training Capabilities E-
160 APPENDIX F: NAVWAR Training Capabilities.
F-
170 APPENDIX G: IIF Basic Operator Training Capabilities.
G-
180 APPENDIX H: IIF Vehicle Advanced Training Capabilities.
H-
190 APPENDIX I IIF Payload Advanced Training Capabilities.
J-1
List of Tables 4Table 1: Requirements Documentation
1Table A-1: Requirements Verification Matrix A-
5Table A-2: Requirements Traceability Matrix A-
1Table B-1: Basic Operator (BOPR) Training Capabilities B-
1Table C-1: Vehicle Advanced Training Capabilities C-
1Table D-1: Payload Advanced Training Capabilities D-
1Table E-1: Crew Advanced Training Capabilities E-
1Table F-1: NAVWAR Training Capabilities F-
1Table G-1: IIF Basic Operator Training Capabilities G-
1Table H-1: IIF Vehicle Advanced Training Capabilities H-
1Table I-1: IIF Payload Advanced Training Capabilities I-
List of Figures
2Figure 1-1. System Diagram
1 Scope
1.1 Identification
This Software Requirements Specification (SRS), MG50539000013E2, specifies the requirements and qualification provisions for the Positional Training Emulator (PTE) computer software. It includes the requirements and qualification provisions for the three components of PTE: the Global Positioning System (GPS) Operational Control System (OCS) Architecture Evolution Program (AEP), the GPS Satellite Training and Rehearsal Simulator (STARSIM) version of the GPS System Simulator, and Instructor Control (IC).
1.2 System Overview
1.2.1 PTE Mission
The mission of the PTE is to provide a realistic training environment for the 50th Operation Support Squadron (OSS) that supports crew training and positional training for the Global Positioning System (GPS) Operational Control System (OCS) operators.
PTE provides a GPS training emulator for the 50th (OSS). It provides the operators of the GPS ground system with realistic Basic Operator Training (BOPR) and Advanced Operator Training that includes Vehicle Advanced, Payload Advanced, Crew Advanced and Navigation Warfare (NAVWAR) training.
PTE is a tailored combination of the Global Positioning System (GPS) Operational Control System (OCS) Architecture Evolution Program (AEP), the GPS Satellite Training and Rehearsal (STAR) Simulator (SIM), and the Instructor Control (IC). See Figure 1-1.
Figure 1-1. System Diagram
1.2.2 PTE Software Overview
1.3 Document Overview
The purpose of this Software Requirements Specification (SRS) is to specify the requirements and qualification provisions of the PTE. The remaining paragraphs of this specification contain a list of referenced documents, the computer software requirements, the qualification provisions, requirements traceability linking the requirements specified in this SRS with the requirements specified in SS-PTE-615, and Appendix A, which includes a Verification Cross Reference Matrix (VCRM). This document is unclassified. Distribution and destruction of this document should follow the instructions specified on the title page of this document.
1.3.1 Document Requirements Terminology and Use
This specification and its supporting/subordinate specifications utilize the following requirements terminology:
a. A 'shall' identifies a requirement (or any portion thereof) that is being designed, built and unless otherwise stated, tested. Each 'shall' is uniquely numbered for identification and traceability.
b. A 'must' identifies a requirement that is not being designed, built or tested, but is a system design constraint or provision that is being provided to the designer by the government (upon which the designer is dependent). 'Musts' are not numbered, and thus there is no provision for unique identification or traceability.
c. The conventional usage of 'wills' for government furnished equipment/property (GFE/GFP) etc., is now handled as described above (now using 'musts'), except in the cases where the portion of the system being designed is not dependent upon the GFE/GFP (which is identified by the use of 'will'). 'Wills' are not numbered, and thus there is no provision for unique identification or traceability.
2 Referenced Documents
2.1 Government Documents
Interim Department of Defense (DoD) Certification and Accreditation (C&A) Process Guidance, SUBJECT: DoD Information Assurance Certification and Accreditation Process (DIACAP), Undated (distributed July 2006)
DoD Directive 8500.1, SUBJECT: Information Assurance (IA), October 24, 2002
DoD Instruction 8500.2, SUBJECT: Information Assurance (IA) Implementation, February 6, 2003
2.1.1 Specifications
2.1.1.1 Federal
2.1.1.2 Military
None.
2.1.1.3 Other Government Documents
None.
2.1.2 Standards
2.1.2.1 Federal
None.
2.1.2.2 Military
None.
2.1.2.3 Other Government Documents
Interim Department of Defense (DoD) Certification and Accreditation (C&A) Process Guidance, SUBJECT: DoD Information Assurance Certification and Accreditation Process (DIACAP), Undated (distributed July 2006)
DoD Directive 8500.1, SUBJECT: Information Assurance (IA), October 24, 2002 DoD Instruction 8500.2, SUBJECT: Information Assurance (IA) Implementation, February 6, 2003
2.1.3 Drawings
None.
2.1.4 Other Publications
2.1.4.1 Manuals
None.
2.1.4.2 Regulations
None.
2.1.4.3 Handbooks
None.
2.1.4.4 Bulletins
None.
2.2 Non-government Documents
2.2.1 Reference Documents
Table 1: Requirements Documentation
MG50539000013E5
Rev NEW Interface Design Document for the Positional Training Emulator of the Global Positioning System Block IIF
MG50533001033E2
Rev A Software Requirements Specification for the System Simulator CSCI of the Global Positioning System Block IIF-Rel 3
SS-PTE-615
Rev B Prime Item Development Specification for the Positional Training Emulator of the Global Positioning System Block IIF
MG50532004033E5 Rev A
Software Design Document for the Telemetry, Tracking and Command CSCI of the Global Positioning System Block IIF-V5.5
MG50532004033E2 Rev D
Software Requirements Specification for the Telemetry, Tracking and Command CSCI of the Global Positioning System Block IIF-V5.5
2.2.2 Specifications
None.
2.2.3 Standards
X Window System
Version 11, Release 6 X Window System
| OSF Motif Version 1.2 |
| Open Software Foundation Motif |
2.2.4 Drawings
2.2.5 Other Publications
3 Requirements
3.1 Required States and Modes.
| PTE-SRS-3221 |
| During the Scenario Preparation State, the PTE shall permit the Instructor to create and modify scenario scripts. The script tool shall be able to create, save, recall and edit scripts. The script shall consist of directives that control the behavior of the Sim and AEP components. The script tool shall support script composition using menus and pick lists. |
| PTE-SRS-3222 |
| During the Scenario Execution State, the PTE shall permit the instructor to control script execution. The script shall provide the automatic execution of a list of directives that control the behavior of the AEP and Sim components. PTE script execution control shall provide the following during a training scenario: |
· Support the independent execution of a script for each student
· Perform sequential execution of directives
· Delay directive execution a specified interval of simulation time after completion of the previous directive
· Delay directive execution a specified interval of simulation time since the start of the scenario
· Include in the script a pause for script execution
· Allow a script to invoke another script
· Permit the instructor to pause script execution
· Permit the instructor to step through the execution of a script
· Permit the instructor to go to any directive in the script to resume script execution from that directive
· Permit the instructor to select, specify, and execute a directive during a training scenario
3.2 Software System Requirements.
3.2.1 Hardware
| PTE-SRS-3235 |
| PTE shall provide software to control the date/time display that provides the simulation time for training scenarios. The PTE date/time will be displayed as YYYY/DDD/HH:MM:SS.sss. |
| PTE-SRS-3236 |
| PTE shall display Space Vehicle (SV) media manager data on the third Common Operator Support Environment (COSE) workstation display monitor. |
3.2.2 PTE Capability Requirements
| PTE-SRS-3238 |
| PTE shall permit the instructor to control the startup and shutdown of the PTE. |
| PTE-SRS-3239 |
| PTE shall provide software that is capable of executing on the PTE MCS and GSS consolidated server platform. |
| PTE-SRS-3240 |
| PTE shall emulate operational MCS TT&C processing associated with SV contacts. |
| PTE-SRS-3241 |
| PTE shall provide updates to telemetry displays that emulate the updates of telemetry displays in the operational MCS. |
| PTE-SRS-3242 |
| PTE shall emulate SV commanding and upload/load transmissions in the operational MCS. |
| PTE-SRS-3243 |
| PTE shall emulate keyboard "look and feel" of the operational MCS. |
| PTE-SRS-3244 |
| PTE shall provide real time responses to operator inputs that emulate operational MCS responses. |
| PTE-SRS-3245 |
| PTE shall emulate the appearance and behavior of the operator displays of the operational MCS. |
| PTE-SRS-3246 |
| PTE shall provide operator display response times comparable to the operational MCS. |
| PTE-SRS-3247 |
| PTE shall provide the capability to include the following block types of simulated GPS SVs in the constellation used for training: IIA, IIR, IIR-M, and IIF. |
| PTE-SRS-3248 |
| PTE shall provide the capability to simulate the following types of ground stations: GA/MS, MS only, Automated Remote Tracking Station (ARTS), National Geospatial-Intelligence Agency (NGA MS). |
| PTE-SRS-3249 |
| PTE shall provide the capability to ghost operator directives for operator positions not being trained during the execution of a training scenario. Ghosting is defined as: automated tasks that would normally be performed by a position that is not part of a scenario (i.e., provide scripts, directives and perform files) |
| PTE-SRS-3250 |
| PTE shall provide the capability to simulate up to 10 OCS ground sites at a time, selected from the 16 OCS ground sites supported by the MCS. The 16 OCS ground sites defined for PTE are as follows: 4 OCS Ground Antenna/Monitoring Station (GA/MS), 2 OCS MS, cloned 10 ARTS sites and 10 PTE cloned OCS GA/MS. Crew scenarios use the 4 OCS GA/MS & 2 OCS MS; Positional scenarios use the 10 PTE cloned OCS GA/MS or cloned ARTS. |
| PTE-SRS-3761 |
| PTE shall have an additional Operating System Status Monitor that will be used for monitoring system level processes (loads, shutdowns, and hangs). |
| PTE-SRS-3762 |
| PTE shall have the capability to switch between Run Level 3 and 4. |
| PTE-SRS-3763 |
| PTE shall have a System Start-Up Status Window that will provide system status monitoring as training scenarios are being conducted. |
| PTE-SRS-3764 |
| PTE shall have a Repeatability Scenario Monitor Window that will monitor the manipulation of push buttons and the status of processes. |
| PTE-SRS-3765 |
| PTE shall have an additional Sim Status Monitor Window that will monitor the PTE Simulation component for status of push buttons and process. |
| PTE-SRS-3766 |
| PTE shall have an additional System Shutdown Display Window that will provide the capability to view processes/applications that are hung-up or have been shut down. |
3.2.2.1 Scenario Execution.
| PTE-SRS-3252 |
| The PTE MCS component shall respond to IC component directives when requested. |
3.2.2.2 Initial Conditions and Time Synchronization.
| PTE-SRS-3254 |
| PTE shall provide the capability to initialize a training session to a specific set of initial conditions. |
| PTE-SRS-3255 |
| The PTE Sim shall provide a simulation time (scenario) to Instructor Control and MCS. |
| PTE-SRS-3256 |
| Instructor Control and MCS shall maintain their time to be consistent with the time provided by Sim (scenario) time. |
3.2.2.3 Pause/Resume Time Operations.
| PTE-SRS-3258 |
| PTE shall have the capability to pause and resume simulated time upon request from the IC component. |
3.2.2.4 Fast/Slow Time Operations
| PTE-SRS-3260 |
| PTE shall provide multiple fast forward speeds of 0.5x, 2x, 3x, 5x, or 10x; all of which represent multiples of normal processing speed (e.g., "2x" indicated two times normal processing speed). |
3.2.2.5 Save/Restore Operations.
| PTE-SRS-3262 |
| PTE shall provide the capability to save the current training session. |
| PTE-SRS-3263 |
| PTE shall provide the capability to restore (load) a previously saved training session. |
3.2.2.6 Logging of Student Activities.
| PTE-SRS-3265 |
| PTE shall provide logging of student activities for instructor viewing. |
| PTE-SRS-3266 |
| PTE shall associate a student position with log messages in the Instructor Control logs. |
| PTE-SRS-3267 |
| PTE shall provide a status parameter value for log messages in Instructor Control logs. |
| PTE-SRS-3268 |
| PTE shall provide a time stamp value for log messages in the Instructor Control logs. |
| PTE-SRS-3269 |
| PTE shall provide log messages which capture startup and shutdown status in the Instructor Control logs |
| PTE-SRS-3270 |
| PTE shall provide log messages in the Instructor Control logs related to: execution of Operational Perform Files, identifying Perform File entry, Perform File exit, and Perform File input parameter values. |
| PTE-SRS-3271 |
| PTE shall provide log messages in Instructor Control logs displayed in the MCS GGI (GPS Graphical Interface) message bins. |
| PTE-SRS-3272 |
| PTE shall provide log messages in Instructor Control logs containing MCS MMS (Message Monitor Scroll) messages displayed in the contact bin. |
3.2.2.7 Initial Condition Management
3.2.2.7.1 Initial Condition Data Management.
| PTE-SRS-3275 |
| Upon request, PTE shall provide the names of currently saved PTE MCS scenarios (state saves) to the IC component. |
| PTE-SRS-3276 |
| PTE shall initialize the PTE MCS from a specified saved checkpoint (full load) to create the initial conditions for synchronization with the SIM component upon request from the IC component. |
| PTE-SRS-3277 |
| PTE shall delete a specified checkpoint (full save) upon request from the IC component. |
3.2.2.7.2 Initial Condition Data Synchronization.
| PTE-SRS-3279 |
| PTE shall provide the scenario start time of the PTE MCS checkpoint being used for synchronization with the SIM component upon request from the SIM component. |
| PTE-SRS-3280 |
| PTE shall provide the SV numbers of the operational SVs in the PTE MCS checkpoint being used for synchronization with the SIM component upon request from the SIM component. |
| PTE-SRS-3281 |
| PTE shall provide synchronization data for a specified SV in the PTE MCS checkpoint being used for synchronization with the SIM component upon request from the SIM component. |
| PTE-SRS-3282 |
| PTE shall provide synchronization data for a specified Remote Site (GA or MS) in the PTE MCS checkpoint being used for synchronization with the SIM component upon request from the SIM component. |
3.2.3 Crew Training.
| PTE-SRS-3284 |
| PTE shall provide the capability to train up to seven crew positions made up of (1) Mission Commander (MC), (1) Mission Chief (MCH), (2) Space System Operators (SSO), (1) Space Vehicle Officer (SVO), (1) Payload Systems Officer (PSO) and (1) Navigation Warfare Officer (NWO). |
3.2.4 Positional Training
| PTE-SRS-3286 |
| PTE shall allow multiple SVs in the simulated constellation to share orbital and physical properties. |
| PTE-SRS-3287 |
| PTE shall allow multiple ground stations to share location and physical properties. |
| PTE-SRS-3288 |
| PTE shall provide the capability to perform up to 10 simultaneous contacts. |
3.2.5 Basic Operator (BOPR) Training
| PTE-SRS-3290 |
| PTE shall provide the capability to execute BOPR training scenarios for Block IIA/IIR/IIF SVs per Appendix B Basic Operator Training Capabilities and Appendix G IIF Basic Operator Training Capabilities. |
3.2.6 Advanced Training Capabilities (Advanced Operator Training).
| PTE-SRS-3292 |
| PTE shall provide the capability to execute Vehicle Advanced training scenarios for Block IIA/IIR/IIF SVs per Appendix C Vehicle Advanced Training Capabilities and Appendix H IIF Vehicle Advanced Training Capabilities |
| PTE-SRS-3293 |
| PTE shall provide the capability to execute Payload Advanced training scenarios for Block IIA/IIR/IIF SVs per Appendix D Payload Advanced Training Capabilities and Appendix I IIF Payload Advanced Training Capabilities. Certain scenarios will contain steps that cannot be performed simultaneously by multiple students. |
| PTE-SRS-3294 |
| PTE shall provide the capability to execute Crew Advanced training scenarios for Block IIA/IIR/IIF SVs per Appendix E Crew Advanced Training Capabilities. Certain scenarios will contain steps that cannot be performed simultaneously by multiple students. |
| PTE-SRS-3662 |
| PTE shall provide the capability to execute Navigation Warfare (NAVWAR) training capabilities for Block IIA/IIR and IIF SVs per Appendix F NAVWAR Training Capabilities. Certain scenarios will contain steps that cannot be performed simultaneously by multiple students. |
3.2.7 PTE MCS External Interface Requirements.
N/A
3.3.1 Interface Identification and Diagrams.
| PTE-SRS-3298 |
| The PTE MCS shall interface with the SIM component as described in the PTE Interface Design Document (IDD), the TTC SDD Appendix F, and applicable OCS Interface Control Documents (ICDs). |
| PTE-SRS-3299 |
| The PTE MCS shall have an interface with the IC component as described in the PTE IDD. |
| PTE-SRS-3300 |
| The PTE shall have an interface between the SIM and IC components as described in the PTE IDD. |
3.3.2 Project Unique Identification of Interface.
This section has been tailored out.
3.3.3 PTE MCS System External Interface Requirements.
N/A
3.4 PTE Internal Interface Requirements.
All internal interfaces of the PTE have been left to design.
3.5 PTE Internal Data Requirements.
All decisions about the internal data of the PTE have been left to design.
3.6 Adaptation Requirements.
This section is not applicable to this SRS.
3.7 Safety Requirements.
This section is not applicable to this SRS.
3.8 Security and Privacy Requirements.
| PTE-SRS-3314 |
| The PTE shall comply with the following: |
• Interim Department of Defense (DoD) Certification and Accreditation (C&A) Process Guidance, SUBJECT: DoD Information Assurance Certification and Accreditation Process (DIACAP), Undated (distributed July 2006)
• DoD Directive 8500.1, SUBJECT: Information Assurance (IA), October 24, 2002
• DoD Instruction 8500.2, SUBJECT: Information Assurance (IA) Implementation, February 6, 2003
3.9 PTE Environment Requirements.
The PTE operates in the environment provided by the Services Computer Software Configuration Item (CSCI) of the OCS.
3.10 Computer Resource Requirements.
3.10.1 Computer Hardware Requirements.
This section is not applicable to this SRS.
3.10.2 Computer Hardware Resource Utilization Requirements.
This section has been tailored out.
3.10.3 Computer Software Requirements.
The PTE uses the services of the computer software provided by the Services CSCI of the OCS.
3.10.4 Communications Requirements.
The PTE uses the computer communication services of the OCS Services CSCI.
3.11 Software Quality Factors.
This section has been tailored out.
3.12 Design and Implementation Constraints.
The PTE Design is accomplished by reuse of the real AEP Command and Control system in conjunction with the existing Simulator (GPSS). The PTE Simulator component reuses GPSS satellite and ground antenna models. By default, this technical solution provides the look and behavior of the operational AEP system. The GPSS Space Segment, GA, MS, and ARTS model requirements have been previously qualified and accepted.
GPSW and 50th Space Wing accept the fact that there will be some compromise in PTE usability as a result of their selection of the AEP-Centric Option, November 2006 (as presented by Boeing in the last of the AEP PTE Solution briefings). The trade-off with the AEP-Centric solution option is better fidelity and lower technical risk, versus a potential compromise in usability (unlimited student independence whereby each student trains in their own GPS universe.
3.13 Personnel Related Requirements.
This section has been tailored out.
3.14 Training Related Requirements.
This section has been tailored out.
3.15 Logistics Related Requirements.
This section is not applicable to this SRS.
3.16 Other Requirements.
This section is not applicable to this SRS.
3.17 Packaging Requirements.
This section is not applicable to this SRS.
3.18 Precedence and Criticality of Requirements.
This section is not applicable to this SRS.
4 Qualification Provisions
PTE verification demonstrations of the capabilities are performed with Air Force participation.
The Air Force performance worksheet training scenarios are used as test procedures. The verification method for requirements in this document (Table B-1) will be verified through demonstration.
Exception: Test procedures or scripts shall be used to demonstrate the set of Training Features.
Verification Sheets (VS) are generated prior to each capability demonstration, which concisely describes how each capability is demonstrated. The VS is signed before and after each demonstration to document the agreement between the Air Force and Boeing. Signed VS are impounded by Quality Assurance (QA).
All demonstrations will be conducted at the Boeing GPS Center, witnessed by the 50th OSS, GPSW, and Boeing QA.
The following are accomplished for rapid prototype test and verification activities:
· Develop and exercise training scenarios as the system develops
· Obtain Air Force concurrence throughout the process (not just at the end)
· Air Force participation in development and exercise of training scenarios
· Reconcile system functionality with capabilities list
· The Air Force will rate the training tasks performance based on pass/fail
· Boeing QA will witness demonstrations
· Discrepancies will be noted during demonstrations
· If necessary, software will be updated between individual capability demonstrations to achieve a passing rating.
4.1 Test Program
The contractor's test program will qualify each requirement in Table A-1, Requirements Traceability and Verification Cross Reference, by the specified method.
4.2 Verification Methods
4.2.1 Demonstration.
The demonstration method is the operation of the system, or a part of the system that relies on observable functional operation not requiring the use of instrumentation, special test equipment, or subsequent analysis.
4.2.2 Test.
The test method is the operation of the system, or a part of the system, using instrumentation or other special test equipment to collect data for later analysis.
4.2.3 Analysis.
The analysis method is the analytical processing of accumulated data obtained from studies, calculations, analysis, modeling and/or other qualification methods. Examples are reduction, interpolation, or extrapolation of test results.
4.2.4 Inspection.
The inspection method is the visual examination of system components, documentation, etc.
5 Requirements Traceability
See Appendix A 6 Notes
6.1 Acronyms
| 2SOPS |
| Second Space Operations Squadron |
| ABTCU |
| Active Base Plate Thermal Control Unit |
| AEP |
| Architecture Evolution Plan |
| AMMM |
| Autonomous Magnetic Momentum Management |
| ARTS |
| Automated Remote Tracking Station |
| ATO |
| Authorization to Operate |
| BDD |
| Burst Detector Dosimeter |
| C&A |
| Certification and Accreditation |
| COSE |
| Common Operator Support Environment |
| COTS |
| Commercial Off-The-Shelf |
| CSCD |
| Control System Command Decoder |
| CSCI |
| Computer Software Configuration Item |
| CTDU |
| Crosslink Transponder Data Unit |
| CTO |
| Command Tasking Order |
| DCEA |
| Digital Control Electronics Assembly |
| DIACAP |
| DoD Information Assurance Certification and Accreditation Process |
| DoD |
| Department of Defense |
| EAROM |
| Electrically Alterable Read-Only Memory |
| FQT |
| Formal Qualification Test |
| GBD |
| Global Burst Detector |
| GFE |
| Government Furnished Equipment |
| GFP |
| Government Furnished Property |
| GGI |
| GPS Graphical Interface |
| GPS |
| Global Positioning System |
| GUV |
| Group Unique Variable |
| HANU |
| High Accuracy Navigation Users |
| ICD |
| Interface Control Document |
| IDD |
| Interface Design Document |
| IPTR |
| In-Process Technical Review |
| ITS |
| Integrated Transfer System |
| MCS |
| Master Control Station |
| MMS |
| Message Monitor Scroll |
| MOX |
| Mission Operations Transfer |
| NAVWAR |
| Navigation Warfare |
| NGA |
| National Geospatial-Intelligence Agency |
| NDS |
| Nuclear Detonation (NUDET) Detection System |
| NDU |
| Navigational Data Unit |
| NWO |
| Navigation Warfare Officer |
| OCS |
| Operational Control Segment |
| OSF |
| Open Software Foundation |
| OSS |
| Operational Support Squadron |
| PIDS |
| Prime Item Development Specification |
| PRR |
| Pseudo Range Residuals |
| PSO |
| Payload Systems Officer |
| PTE |
| Positional Training Emulator |
| RCS |
| Reaction Control Subsystem |
| RFDU |
| Radio Frequency Digital Unit |
| RWA |
| Reaction Wheel Assembly |
| SAASM |
| Selective Availability and Anti-Spoofing Module |
| SADPT |
| Solar Array Drive and Power Transfer Assembly |
| SDD |
| Software Design Description |
| SIP |
| SAASM Implementation Plan |
| SOO |
| Statement of Objectives |
| SPU |
| Spacecraft Processor Unit |
| SRS |
| Software Requirement Specification |
| SSO |
| Space System Operator |
| STD |
| Software Test Description |
| STARSIM |
| Satellite Training and Rehearsal Simulator |
| SVMM |
| Satellite Vehicle Media Manager |
| SVO |
| Space Vehicle Officer |
| TIU |
| Telemetry Interface Unit |
| TT&C |
| Telemetry, Tracking and Control |
| USNO |
| United States Naval Observatory |
| VCC |
| Vehicle Command Count |
| VCRM |
| Verification Cross Reference Matrix |
| WGMIC |
| Waveform Generator, Modulator, Intermediate Power Amplifier, and DC/DC Converter |
6.2 Technical Glossary
10 APPENDIX A: Requirements Traceability and Verification Cross Reference Table A-1: Requirements Verification Matrix
| Object Identifier |
| New Para |
| RVM_A |
| RVM_D |
| RVM_I |
| RVM_T |
| PTE-SRS-3221 |
| 3.1 Required States and Modes |
X
| PTE-SRS-3222 |
| 3.1 Required States and Modes |
X
| PTE-SRS-3235 |
| 3.2.1 Hardware |
X
| PTE-SRS-3236 |
| 3.2.1 Hardware |
X
| PTE-SRS-3238 |
| 3.2.2 PTE Capability Requirements |
X
| PTE-SRS-3239 |
| 3.2.2 PTE Capability Requirements |
X
| PTE-SRS-3240 |
| 3.2.2 PTE Capability Requirements |
X
| PTE-SRS-3241 |
| 3.2.2 PTE Capability Requirements |
X
| PTE-SRS-3242 |
| 3.2.2 PTE Capability Requirements |
X
| PTE-SRS-3243 |
| 3.2.2 PTE Capability Requirements |
X
| PTE-SRS-3244 |
| 3.2.2 PTE Capability Requirements |
X
| PTE-SRS-3245 |
| 3.2.2 PTE Capability Requirements |
X
| PTE-SRS-3246 |
| 3.2.2 PTE Capability Requirements |
X
| PTE-SRS-3247 |
| 3.2.2 PTE Capability Requirements |
X
| PTE-SRS-3248 |
| 3.2.2 PTE Capability Requirements |
X
| PTE-SRS-3249 |
| 3.2.2 PTE Capability Requirements |
X
| PTE-SRS-3250 |
| 3.2.2 PTE Capability Requirements |
X
| PTE-SRS-3761 |
| 3.2.2 PTE Capability Requirements |
X
| PTE-SRS-3762 |
| 3.2.2 PTE Capability Requirements |
X
| PTE-SRS-3763 |
| 3.2.2 PTE Capability Requirements |
X
| PTE-SRS-3764 |
| 3.2.2 PTE Capability Requirements |
X
| PTE-SRS-3765 |
| 3.2.2 PTE Capability Requirements |
X
| PTE-SRS-3766 |
| 3.2.2 PTE Capability Requirements |
X
| PTE-SRS-3252 |
| 3.2.2.1 Scenario Execution. |
X
| PTE-SRS-3254 |
| 3.2.2.2 Initial Conditions and Time Synchronization. |
X
| PTE-SRS-3255 |
| 3.2.2.2 Initial Conditions and Time Synchronization. |
X
| PTE-SRS-3256 |
| 3.2.2.2 Initial Conditions and Time Synchronization. |
X
| PTE-SRS-3258 |
| 3.2.2.3 Pause/Resume Time Operations. |
X
| PTE-SRS-3260 |
| 3.2.2.4 Fast/Slow Time Operations |
X
| PTE-SRS-3262 |
| 3.2.2.5 Save/Restore Operations. |
X
| PTE-SRS-3263 |
| 3.2.2.5 Save/Restore Operations. |
X
| PTE-SRS-3265 |
| 3.2.2.6 Logging of Student Activities. |
X
| PTE-SRS-3266 |
| 3.2.2.6 Logging of Student Activities. |
X
| PTE-SRS-3267 |
| 3.2.2.6 Logging of Student Activities. |
X
| PTE-SRS-3268 |
| 3.2.2.6 Logging of Student Activities. |
X
| PTE-SRS-3269 |
| 3.2.2.6 Logging of Student Activities. |
X
| PTE-SRS-3270 |
| 3.2.2.6 Logging of Student Activities. |
X
| PTE-SRS-3271 |
| 3.2.2.6 Logging of Student Activities. |
X
| PTE-SRS-3272 |
| 3.2.2.6 Logging of Student Activities. |
X
| PTE-SRS-3275 |
| 3.2.2.7.1 Initial Condition Data Management. |
X
| PTE-SRS-3276 |
| 3.2.2.7.1 Initial Condition Data Management. |
X
| PTE-SRS-3277 |
| 3.2.2.7.1 Initial Condition Data Management. |
X
| PTE-SRS-3279 |
| 3.2.2.7.2 Initial Condition Data Synchronization. |
X
| PTE-SRS-3280 |
| 3.2.2.7.2 Initial Condition Data Synchronization. |
X
| PTE-SRS-3281 |
| 3.2.2.7.2 Initial Condition Data Synchronization. |
X
| PTE-SRS-3282 |
| 3.2.2.7.2 Initial Condition Data Synchronization. |
X
| PTE-SRS-3284 |
| 3.2.3 Crew Training. |
X
| PTE-SRS-3286 |
| 3.2.4 Positional Training |
X
| PTE-SRS-3287 |
| 3.2.4 Positional Training |
X
| PTE-SRS-3288 |
| 3.2.4 Positional Training |
X
| PTE-SRS-3290 |
| 3.2.5 Basic Operator (BOPR) Training |
X
| PTE-SRS-3292 |
| 3.2.6 Advanced Training Capabilities (Advanced Operator Training) |
X
| PTE-SRS-3293 |
| 3.2.6 Advanced Training Capabilities (Advanced Operator Training) |
X
| PTE-SRS-3294 |
| 3.2.6 Advanced Training Capabilities (Advanced Operator Training) |
X
| PTE-SRS-3662 |
| 3.2.6 Advanced Training Capabilities (Advanced Operator Training) |
X
| PTE-SRS-3298 |
| 3.3.1 Interface Identification and Diagrams. |
X
| PTE-SRS-3299 |
| 3.3.1 Interface Identification and Diagrams. |
X
| PTE-SRS-3300 |
| 3.3.1 Interface Identification and Diagrams. |
X
| PTE-SRS-3314 |
| 3.8 Security and Privacy requirements. |
Table A-2: Requirements Traceability Matrix
| Object Identifier |
| Paragraph ID |
| New Para Heading Only |
| PTE PIDS ID |
| PTE PIDS Paragraph No. |
| PTE-SRS-3221 |
| 3.1 |
| Required States and Modes |
| SS-PTE-34 |
| 3.1.1 |
| PTE-SRS-3222 |
| 3.1 |
| Required States and Modes |
| SS-PTE-34 |
| 3.1.1 |
| PTE-SRS-3235 |
| 3.2.1 |
| Hardware |
| SS-PTE-36 |
| 3.1.3 |
| PTE-SRS-3236 |
| 3.2.1 |
| Hardware |
| SS-PTE-36 |
| 3.1.3 |
| PTE-SRS-3238 |
| 3.2.2 |
| PTE Capability Requirements |
| SS-PTE-39 |
| 3.1.6 |
| PTE-SRS-3239 |
| 3.2.2 |
| PTE Capability Requirements |
| SS-PTE-44 |
| 3.2.1.2 |
| PTE-SRS-3240 |
| 3.2.2 |
| PTE Capability Requirements |
| SS-PTE-54 |
| 3.2.2 |
| PTE-SRS-3241 |
| 3.2.2 |
| PTE Capability Requirements |
| SS-PTE-54 |
| 3.2.2 |
| PTE-SRS-3242 |
| 3.2.2 |
| PTE Capability Requirements |
| SS-PTE-54 |
| 3.2.2 |
| PTE-SRS-3243 |
| 3.2.2 |
| PTE Capability Requirements |
| SS-PTE-54 |
| 3.2.2 |
| PTE-SRS-3244 |
| 3.2.2 |
| PTE Capability Requirements |
| SS-PTE-54 |
| 3.2.2 |
| PTE-SRS-3245 |
| 3.2.2 |
| PTE Capability Requirements |
| SS-PTE-54 |
| 3.2.2 |
| PTE-SRS-3246 |
| 3.2.2 |
| PTE Capability Requirements |
| SS-PTE-54 |
| 3.2.2 |
| PTE-SRS-3247 |
| 3.2.2 |
| PTE Capability Requirements |
| SS-PTE-56 |
| 3.2.3 |
| PTE-SRS-3248 |
| 3.2.2 |
| PTE Capability Requirements |
| SS-PTE-56 |
| 3.2.3 |
| PTE-SRS-3249 |
| 3.2.2 |
| PTE Capability Requirements |
| SS-PTE-54 |
| 3.2.2 |
| PTE-SRS-3250 |
| 3.2.2 |
| PTE Capability Requirements |
| SS-PTE-56 |
| 3.2.3 |
| PTE-SRS-3761 |
| 3.2.2 |
| PTE Capability Requirements |
| SS-PTE-54 |
| 3.2.3 |
| PTE-SRS-3762 |
| 3.2.2 |
| PTE Capability Requirements |
| SS-PTE-54 |
| 3.2.3 |
| PTE-SRS-3763 |
| 3.2.2 |
| PTE Capability Requirements |
| SS-PTE-54 |
| 3.2.3 |
| PTE-SRS-3764 |
| 3.2.2 |
| PTE Capability Requirements |
| SS-PTE-54 |
| 3.2.3 |
| PTE-SRS-3765 |
| 3.2.2 |
| PTE Capability Requirements |
| SS-PTE-54 |
| 3.2.3 |
| PTE-SRS-3766 |
| 3.2.2 |
| PTE Capability Requirements |
| SS-PTE-54 |
| 3.2.3 |
| PTE-SRS-3252 |
| 3.2.2.1 |
| Scenario Execution. |
| SS-PTE-71 |
| 3.2.7.4 |
| PTE-SRS-3254 |
| 3.2.2.2 |
| Initial Conditions and Time Synchronization. |
| SS-PTE-77 |
| 3.2.7.7 |
| PTE-SRS-3255 |
| 3.2.2.2 |
| Initial Conditions and Time Synchronization. |
| SS-PTE-77 |
| 3.2.7.7 |
| PTE-SRS-3256 |
| 3.2.2.2 |
| Initial Conditions and Time Synchronization. |
| SS-PTE-77 |
| 3.2.7.7 |
| PTE-SRS-3258 |
| 3.2.2.3 |
| Pause/Resume Time Operations. |
| SS-PTE-79 |
| 3.2.7.8 |
| PTE-SRS-3260 |
| 3.2.2.4 |
| Fast/Slow Time Operations |
| SS-PTE-81 |
| 3.2.7.9 |
| PTE-SRS-3262 |
| 3.2.2.5 |
| Save/Restore Operations. |
| SS-PTE-83 |
| 3.2.7.10 |
| PTE-SRS-3263 |
| 3.2.2.5 |
| Save/Restore Operations. |
| SS-PTE-83 |
| 3.2.7.10 |
| PTE-SRS-3265 |
| 3.2.2.6 |
| Logging of Student Activities. |
| SS-PTE-85 |
| 3.2.7.11 |
| PTE-SRS-3266 |
| 3.2.2.6 |
| Logging of Student Activities. |
| SS-PTE-85 |
| 3.2.7.11 |
| PTE-SRS-3267 |
| 3.2.2.6 |
| Logging of Student Activities. |
| SS-PTE-85 |
| 3.2.7.11 |
| PTE-SRS-3268 |
| 3.2.2.6 |
| Logging of Student Activities. |
| SS-PTE-85 |
| 3.2.7.11 |
| PTE-SRS-3269 |
| 3.2.2.6 |
| Logging of Student Activities. |
| SS-PTE-85 |
| 3.2.7.11 |
| PTE-SRS-3270 |
| 3.2.2.6 |
| Logging of Student Activities. |
| SS-PTE-85 |
| 3.2.7.11 |
| PTE-SRS-3271 |
| 3.2.2.6 |
| Logging of Student Activities. |
| SS-PTE-85 |
| 3.2.7.11 |
| PTE-SRS-3272 |
| 3.2.2.6 |
| Logging of Student Activities. |
| SS-PTE-85 |
| 3.2.7.11 |
| PTE-SRS-3275 |
| 3.2.2.7.1 |
| Initial Condition Data Management. |
| SS-PTE-83 |
| 3.2.7.10 |
| PTE-SRS-3276 |
| 3.2.2.7.1 |
| Initial Condition Data Management. |
| SS-PTE-83 |
| 3.2.7.10 |
| PTE-SRS-3277 |
| 3.2.2.7.1 |
| Initial Condition Data Management. |
| SS-PTE-83 |
| 3.2.7.10 |
| PTE-SRS-3279 |
| 3.2.2.7.2 |
| Initial Condition Data Synchronization. |
| SS-PTE-77 |
| 3.2.7.7 |
| PTE-SRS-3280 |
| 3.2.2.7.2 |
| Initial Condition Data Synchronization. |
| SS-PTE-77 |
| 3.2.7.7 |
| PTE-SRS-3281 |
| 3.2.2.7.2 |
| Initial Condition Data Synchronization. |
| SS-PTE-77 |
| 3.2.7.7 |
| PTE-SRS-3282 |
| 3.2.2.7.2 |
| Initial Condition Data Synchronization. |
| SS-PTE-77 |
| 3.2.7.7 |
| PTE-SRS-3284 |
| 3.2.3 |
| Crew Training. |
| SS-PTE-35 |
| 3.1.2 |
| PTE-SRS-3286 |
| 3.2.4 |
| Positional Training |
| SS-PTE-92, SS-PTE-94 |
| 3.2.8.3, 3.2.8.4 |
| PTE-SRS-3287 |
| 3.2.4 |
| Positional Training |
| SS-PTE-92, SS-PTE-94 |
| 3.2.8.3, 3.2.8.4 |
| PTE-SRS-3288 |
| 3.2.4 |
| Positional Training |
| SS-PTE-92, SS-PTE-94 |
| 3.2.8.3, 3.2.8.4 |
| PTE-SRS-3290 |
| 3.2.5 |
| Basic Operator (BOPR) Training |
| SS-PTE-88 |
| 3.2.8.1 |
| PTE-SRS-3292 |
| 3.2.6 |
| Advanced Training Capabilities (Advanced Operator Training). |
| SS-PTE-90 |
| 3.2.8.2 |
| PTE-SRS-3293 |
| 3.2.6 |
| Advanced Training Capabilities (Advanced Operator Training). |
| SS-PTE-92 |
| 3.2.8.3 |
| PTE-SRS-3294 |
| 3.2.6 |
| Advanced Training Capabilities (Advanced Operator Training). |
| SS-PTE-94 |
| 3.2.8.4 |
| PTE-SRS-3662 |
| 3.2.6 |
| Advanced Training Capabilities (Advanced Operator Training). |
| SS-PTE-243 |
| 3.2.8.5 |
| PTE-SRS-3298 |
| 3.3.1 |
| Interface Identification and Diagrams. |
| SS-PTE-54 |
| 3.2.2 |
| PTE-SRS-3299 |
| 3.3.1 |
| Interface Identification and Diagrams. |
| SS-PTE-54 |
| 3.2.2 |
| PTE-SRS-3300 |
| 3.3.1 |
| Interface Identification and Diagrams. |
| SS-PTE-54 |
| 3.2.2 |
| PTE-SRS-3314 |
| 3.8 |
| Security and Privacy requirements. |
| N/A |
| N/A |
20 APPENDIX B: Basic Operator (BOPR) Training Capabilities Table B-1: Basic Operator (BOPR) Training Capabilities
| Ref No. |
| BOPR Training Task |
| SV Model |
| SVMM Location |
| Checklist |
| Description |
| Additional Details |
| 1 |
| 1.6 Perform Ground Antenna Anomaly Resolution |
| IIA and IIR/IIR-M |
| 5.1.1.2 |
| CL1-2 |
| No Lock |
| IIA and IIR/IIR-M |
| 5.1.1.1 |
| CL1-1 |
| Comm Loss During SV Contact |
| Contractor developed |
| 2 |
| 2.1 Perform Prepass Procedures |
| IIA and IIR/IIR-M |
| 3.1.2.2 |
| CL1-8 |
| Precontact and post contact |
| Was originally listed under 2.2 |
| 3 |
| 2.2 Perform Vehicle Contact |
| IIA and IIR/IIR-M |
| 3.1.2.1 |
| CL1-3 |
| SV Contact |
| IIA and IIR/IIR-M |
| 3.1.2.3 |
| CL1-14 |
| Active/Passive Contact |
| 4 |
| 2.3 Perform Nominal State of Health |
| IIA |
| 3.1.2.4 |
| CL1-16 |
| Block IIA State of Health |
| IIR/IIR-M |
| 3.1.2.4 |
| CL1-17 |
| Block IIR/IIR-M State of Health |
2.6 Perform Nominal Vehicle Commanding
| IIA |
| 3.2.1.1 |
| R20-10 |
| Autonomous Magnetic Momentum Management (AMMM) |
| IIA |
| 3.2.1.9 |
| R20-60 |
| Eclipse Monitor |
| IIA |
| 3.2.1.10 |
| R20-61 |
| Post Eclipse Monitor |
| IIA |
| 3.2.1.15 |
| R20-71 |
| Wheel Reconditioning |
| IIA |
| 3.2.1.19 |
| R20-90 |
| Attitude Collection |
| IIR/IIR-M |
| 3.2.1.6 |
| R20-90 |
| Attitude Collection |
| IIA |
| 3.2.11.2 |
| SR23-3 |
| SVN 37 Solar Array Monitor |
| IIA |
| 3.2.2.4 |
| R21-40 |
| Battery Reconditioning |
| IIA |
| 3.2.2.5 |
| R21-50 |
| Battery Status Monitor |
| IIA |
| 3.2.3.2 |
| R22-20 |
| ATO/CTO/COM Commanding |
| IIA |
| 3.2.3.3 |
| R22-30 |
| Test Command |
| IIR/IIR-M |
| 3.2.1.1 |
| R20R-10 |
| Eclipse Monitor |
| IIR/IIR-M |
| 3.2.1.2 |
| R20R-11 |
| Post Eclipse Monitor |
| IIR/IIR-M |
| 3.2.3.2 |
| R22R-20 |
| Configure ATO/CTO/COM |
| IIA |
| 5.2.9.4 |
| A27-40 |
| NDS Commanded CAL |
| Contractor developed |
| IIR/IIR-M |
| 3.2.3.1 |
| R22R-10 |
| Command Block IIR SV |
| Contractor developed |
| IIA |
| 3.2.11.3 |
| SR23-4 |
| SVN 37 Solar Array Commanding |
(A-Side) Contractor developed
| 6 |
| 2.11 Perform Nominal EPS Commanding |
| IIA |
| 3.2.2.6 |
| R21-51 |
| Battery Depth of Discharge Monitor |
| 7 |
| 2.12 Perform Nominal Telemetry, Tracking, and Control Subsystem Commanding Determination |
| IIA |
| 3.2.3.1 |
| R22-10 |
| GBD/NDU Dump |
| IIA |
| 3.2.4.2 |
| R23-15 |
| Block II/IIA NAV Upload Transmission |
| 8 |
| 2.15 Perform Nominal Spacecraft Processor Commanding |
| IIR/IIR-M |
| 3.2.5.12 |
| R23R-42 |
| Request MDU/CTDU/WGMIC Status Telemetry |
| Added to BOPR per request from 50th OSS |
| 9 |
| 2.17 Perform Nominal Payload Subsystem Commanding |
| IIA |
| 3.2.4.1 |
| R23-10 |
| Nav Buffer Status Message Dump |
| IIA |
| 3.2.6.1 |
| R25-10 |
| NDS Magnitude Commanding |
| IIR/IIR-M |
| 3.2.8.2 |
| R25R-10 |
| GBD Magnitude Commanding |
| IIR/IIR-M |
| 3.2.5.18 |
| R23R-85 |
| Block IIR NAV Upload Transmission |
| Added to BOPR per request from 50th OSS |
| 10 |
| 2.23 Resolve telemetry, Tracking, and Control Anomalous Commanding |
| IIA |
| 5.2.4.4 |
| A22-20 |
| Negative Carrier Acquisition |
| IIR/IIR-M |
| 5.2.4.1 |
| A22R-10 |
| No Downlink |
| IIR/IIR-M |
| 5.2.4.3 |
| A22R-20 |
| No Telemetry on Carrier |
| IIR/IIR-M |
| 5.2.5.3 |
| A29R-14 |
| Clear SPU Error Flag |
| IIA |
| 5.2.4.2 |
| A22-15 |
| Command Reject |
| IIR/IIR-M |
| 5.2.4.2 |
| A22R-15 |
| Command Reject |
| IIR/IIR-M |
| 3.2.5.2 |
| R23R-11 |
| Configure MDU Status Queue |
| Not in original SOO |
| IIA |
| 5.2.4.1 |
| A22-10 |
| Unexpected VCC |
| Contractor developed |
| IIR/IIR-M |
| 5.2.4.12 |
| A22R-70 |
| Unexpected VCC |
| Contractor developed |
| IIA |
| 5.2.10.1 |
| A28-10 |
| W-Logics restart |
| Contractor developed |
| 11 |
| 2.25 Resolve Propulsion System Anomaly |
| IIA |
| 5.2.2.11 |
| A20-70 |
| RCS Tank Safing / Tank Leak |
| 12 |
| 2.27 Resolve Advanced Payload Subsystem Anomaly |
| IIA |
| 5.2.5.3 |
| A23-20 |
| Command SV Untrackable |
| Originally listed under 2.23 |
| 13 |
| 2.28 Resolved ITS Anomalous Commanding |
| IIR/IIR-M |
| 5.2.11.1 |
| A27R-10 |
| Commanded System Test |
| 14 |
| 3.1 Perform Payload Display Checks |
| IIA |
| 3.1.1.1 |
| CL3-1 |
| Crew Changeover |
| 15 |
| 3.11 Perform Navigation Upload Transmission Anomaly Procedures |
| IIA |
| 3.2.4.2 |
| R23-15 |
| Block II/IIA NAV Upload Transmission |
| Was not in original SOO |
| IIA |
| 5.3.4.2 |
| A34-4 |
| Block II/IIA Navigation Upload Transmission Anomaly |
| IIR/IIR-M |
| 5.3.4.2 |
| A34-4 |
| Block IIA and IIR NAV Upload Transmission Anomaly |
| Contractor developed |
| 16 |
| 4.1 Perform Routine Shift Actions |
| IIR/IIR-M |
| 3.2.3.6 |
| R22R-50 |
| Transmit Test Command |
| Contractor developed |
| IIR/IIR-M |
| 3.2.8.16 |
| R25R-90 |
| Daily GBD S-Band Dump |
| Contractor developed |
30 APPENDIX C: Vehicle Advanced Training Capabilities
Table C-1: Vehicle Advanced Training Capabilities
| Ref No |
| VA Task |
| SV Model |
| SVMM Location |
| Checklist |
| Description |
| Additional Details |
| 1 |
| 2.1 Perform Pre-Pass |
| IIA and IIR/IIR-M |
| 3.1.2.2 |
| CL1-8 |
| Precontact and Postcontact Conferences |
| 2 |
| 2.4 Perform Nominal State of Health TLM Verification |
| IIA |
| 3.1.2.4 |
| CL1-16 |
| Block IIA State of Health |
| Same SVMM/Checklists as those used for BOPR Training Task 2.3 Perform Nominal State of Health (reference Table 2, Ref No. 4) |
| IIR/IIR-M |
| 3.1.2.4 |
| CL1-17 |
| Block IIR/IIR-M State of Health |
| 3 |
| 2.6 Perform Nominal Vehicle Commanding |
| IIA |
| 3.2.3.2 |
| R22-20 |
| ATO/CTO/COM Commanding |
| Was listed under 2.12 |
| IIA |
| 3.2.3.5 |
| R22-50 |
| Command Block IIA SV |
| Was listed under 2.12 |
| IIR/IIR-M |
| 3.2.3.5 |
| R22R-40 |
| Select TIU Mode |
| Was listed under 2.12 |
| IIA |
| 3.2.3.3 |
| R22-30 |
| Test Command |
| Was listed under 2.12 |
| IIR/IIR-M |
| 3.2.5.2 |
| R23R-11 |
| Configure MDU Status Queue |
| Was listed under 2.17 |
| IIA |
| 5.2.9.4 |
| A27-40 |
| NDS Commanded Cal |
| Was listed under 2.28 |
| IIA |
| 3.2.1.1 |
| R20-10 |
| Autonomous Magnetic Momentum Management (AMMM) |
| IIA |
| 3.2.1.9 |
| R20-60 |
| Eclipse Monitor |
| IIA |
| 3.2.1.10 |
| R20-61 |
| Post Eclipse Monitor |
| IIA |
| 3.2.1.11 |
| R20-62 |
| Noon Turn Monitor |
| IIA |
| 3.2.1.13 |
| R20-64 |
| Lunar Eclipse Monitor |
| IIA |
| 3.2.1.15 |
| R20-71 |
| Wheel Reconditioning |
| IIA |
| 3.2.1.18 |
| R20-76 |
| Momentum Management with Thrusters |
| IIA |
| 3.2.1.19 |
| R20-90 |
| Attitude Collection |
| IIR/IIR-M |
| 3.2.1.6 |
| R20-90 |
| Attitude Collection |
| IIA |
| 3.2.2.4 |
| R21-40 |
| Battery Reconditioning |
| IIA |
| 3.2.2.5 |
| R21-50 |
| Battery Status Monitor |
| IIA |
| 3.2.1.2 |
| R20-30 |
| Control System Command Decoder (CSCD) |
| 4 |
| 2.6 Perform Nominal Vehicle Commanding (continued) |
| IIA |
| 3.2.8.4 |
| R27-40 |
| Command Next Word of Day |
| IIR/IIR-M |
| 3.2.5.18 |
| R23R-85 |
| Block IIR NAV Upload Transmission |
| IIA |
| 3.2.1.12 |
| 2R20-63 |
| Post Noon Turn Monitor |
| 5 |
| 2.8 Perform Nominal Attitude Control System Commanding |
| IIA |
| 3.2.1.4 |
| R20-41 |
| DCEA Memory Dump |
| IIA |
| 3.2.1.6 |
| R20-43 |
| Semi-Annual DCEA Memory Dump |
| IIA |
| 3.2.1.5 |
| R20-42 |
| DCEA EAROM Bank Selection |
| IIR/IIR-M |
| 3.2.1.4 |
| R20R-20 |
| Select RWA Or Thruster Actuator |
| IIA |
| 3.2.1.1 |
| R20-10 |
| Autonomous Magnetic Momentum Management (AMMM) |
| IIA |
| 3.2.1.2 |
| R20-30 |
| Control System Command Decoder (CSCD) |
| IIA |
| 3.2.1.20 |
| R20-91 |
| Manual Mode-5 Momentum Management With Magnets |
2.11 Perform Nominal Electrical Power Subsystem Commanding
| IIA |
| 3.2.2.1 |
| R21-10 |
| Load Shed Enable/Disable |
| IIA |
| 3.2.2.3 |
| R21-30 |
| Battery Charger On/Off |
| IIA |
| 3.2.2.6 |
| R21-51 |
| Battery Depth of Discharge Monitor |
| IIR/IIR-M |
| 3.2.2.1 |
| R21R-10 |
| Select Block IIR Battery Pressure Monitor |
| IIR/IIR-M |
| 3.2.2.2 |
| R21R-20 |
| Select Block IIR V/T Curves |
| IIR/IIR-M |
| 3.2.2.3 |
| R21R-30 |
| Enable/Disable Power Management Functions |
| IIR/IIR-M |
| 3.2.2.4 |
| R21R-40 |
| Configure Battery For 17 Cell Operation |
| 7 |
| 2.12 Perform TT&C Subsystem Commanding |
| IIA |
| 3.2.3.1 |
| R22-10 |
| GBD/NDU Dump |
| IIR/IIR-M |
| 3.2.3.3 |
| R22R-30 |
| Configure Receiver/KIR |
| IIR/IIR-M |
| 3.2.3.4 |
| R22-40 |
| PRN Ranging On/Off |
| IIR/IIR-M |
| 3.2.3.4 |
| R22R-31 |
| Configure PRN Ranging |
| IIR/IIR-M |
| 3.2.3.6 |
| R22R-50 |
| Transmit Test Command |
| 8 |
| 2.13 Perform Nominal Thermal Control Subsystem Commanding |
| IIA |
| 3.2.5.1 |
| R24-10 |
| ABTCU 1 or 2 Enable |
| IIA |
| 3.2.5.2 |
| R24-11 |
| ABTCU 1 or 2 Temperature Configuration |
| IIR/IIR-M |
| 3.2.6.1 |
| R24R-10 |
| Power On/Off RWA Heater |
| 9 |
| 2.14 Perform Nominal Propulsion Subsystem Commanding |
| IIR/IIR-M |
| 3.2.7.1 |
| R20R-70 |
| Configure RCS ISO-Valves |
| IIR/IIR-M |
| 3.2.7.2 |
| R20R-71 |
| Enable/Disable REA Thrusters |
| IIR/IIR-M |
| 3.2.7.3 |
| R20R-72 |
| Enable/Disable REA Power |
| 10 |
| 2.15 Perform Nominal Spacecraft Processor Commanding |
| IIR/IIR-M |
| 3.2.4.7 |
| R29R-23 |
| Backup Ephemeris Management |
| IIR/IIR-M |
| 3.2.4.8 |
| R29R-30 |
| SPU Dump |
| IIR/IIR-M |
| 3.2.4.10 |
| R29R-40 |
| Enable/Disable Redundancy Manager |
| IIR/IIR-M |
| 3.2.9.3 |
| R26M-55 |
| Reset WGMIC |
| 11 |
| 2.17 Perform Nominal Payload Subsystem Commanding |
| IIA |
| 3.2.4.1 |
| R23-10 |
| NAV Buffer Status Message Dump |
| IIA |
| 3.2.4.5 |
| R23-23 |
| Select NAV Buffer Configuration |
| IIA |
| 3.2.6.1 |
| R25-10 |
| NDS Magnitude Command |
| IIA |
| 3.2.6.5 |
| R25-30 |
| NDS Complex Solar Inhibit Initialization |
| IIA |
| 3.2.6.6 |
| R25-40 |
| NDS Delayed Calibration |
| IIR/IIR-M |
| 3.2.8.2 |
| R25R-10 |
| GBD Magnitude Commanding |
| IIR/IIR-M |
| 3.2.8.5 |
| R25R-30 |
| NDS Complex Solar Outage Adjust |
| IIR/IIR-M |
| 3.2.8.7 |
| R25R-40 |
| GBD Delayed System Test |
| IIR/IIR-M |
| 3.2.8.10 |
| R25R-65 |
| Constellation Status Readout |
| 12 |
| 2.18 Perform Nominal ITS Commanding |
| IIA |
| 3.2.8.1 |
| R27-10 |
| Initialize ITS Processor/Receiver |
| IIR/IIR-M |
| 3.2.10.1 |
| R27R-20 |
| Configure CTDU |
| IIR/IIR-M |
| 3.2.10.2 |
| R27R-30 |
| Power On/Off CTDU Receiver |
| IIR/IIR-M |
| 3.2.10.3 |
| R27R-40 |
| Power On/Off CTDU Transmitter |
| IIR/IIR-M |
| 3.2.10.4 |
| R27R-50 |
| Enable/Disable ITS Crosslink Transmission |
| 13 |
| 2.19 Perform Nominal LBD Commanding |
| IIA |
| 3.2.7.1 |
| R26-10 |
| L1/L2 Reconfigure |
| IIA |
| 3.2.7.3 |
| R26-30 |
| L3 Transmitter Enable/Select |
| 14 |
| 2.21 Perform AVCS Anomalous Commanding |
| IIA |
| 3.2.1.2 |
| R20-30 |
| Control System Command Decoder (CSCD) |
| Reference SVMM Section 2.2.1.1.15: Reconfigure WCL In Event Of Reaction Wheel Failure for details. |
| IIA |
| 5.2.2.1 |
| A20-10 |
| Thruster Backup Control |
| IIA |
| 5.2.2.9 |
| A20-30 |
| Clear Command Verification Logic Reject Flag |
| IIA |
| 5.2.2.10 |
| A20-40 |
| Clear Deadman Timer Trip/Mode Select |
| IIR/IIR-M |
| 5.2.2.1 |
| A20R-10 |
| Configure RWA 3/4 Wheel |
| IIR/IIR-M |
| 5.2.2.4 |
| A20R-30 |
| Static Earth Sensor Assembly Switch |
| IIR/IIR-M |
| 5.2.2.6 |
| A20R-50 |
| Configure Spare Torquer Winding |
| 15 |
| 2.22 Perform EPS Anomalous Commanding |
| IIA |
| 5.2.3.2 |
| A21-20 |
| SADPT Channel Power Transfer |
| IIA |
| 5.2.3.3 |
| A21-21 |
| SADPT Mode Change |
| IIA |
| 5.2.3.4 |
| A21-30 |
| SV Found In Load Shed Condition |
| IIA |
| 5.2.3.6 |
| A21-40 |
| Battery Overtemperature |
| IIR/IIR-M |
| 5.2.3.4 |
| A21R-30 |
| SV Found In Load Shed Condition |
| IIR/IIR-M |
| 5.2.3.5 |
| A21R-40 |
| Configure Battery For 16 Cell Operation |
| 16 |
| 2.23 Resolve TT&C Subsystem Anomaly |
| IIA |
| 5.2.4.1 |
| A22-10 |
| Unexpected VCC |
| IIA |
| 5.2.4.2 |
| A22-15 |
| Command Reject |
| IIA |
| 5.2.4.3 |
| A22-16 |
| NDU Processor Reset Command Reject |
| IIA |
| 5.2.4.4 |
| A22-20 |
| Negative Carrier Acquisition |
| IIR/IIR-M |
| 5.2.4.10 |
| A22R-50 |
| Failed CDU |
| IIR/IIR-M |
| 5.2.4.1 |
| A22R-10 |
| No Downlink |
| IIR/IIR-M |
| 5.2.4.3 |
| A22R-20 |
| No Telemetry On Carrier |
| IIR/IIR-M |
| 5.2.4.12 |
| A22R-70 |
| Unexpected VCC |
| IIA |
| 5.2.10.1 |
| A28-10 |
| W-Logics Restart |
| 17 |
| 2.24 Resolve Thermal Control Subsystem Anomaly |
| IIR/IIR-M |
| 5.2.7.1 |
| A24R-10 |
| Failed On RWA Heater |
| IIA |
| 5.2.7.1 |
| A25-10 |
| BDD Power Up/Down |
| 18 |
| 2.25 Resolve Propulsion Subsystem Anomaly |
| IIA |
| 5.2.2.11 |
| A20-70 |
| RCS Tank Safing |
| IIR/IIR-M |
| 5.2.8.1 |
| A20-70 |
| RCS Tank Safing |
| 19 |
| 2.26 Resolve Spacecraft Processor Subsystem Anomaly |
| IIR/IIR-M |
| 5.2.5.8 |
| A29R-50 |
| Clear State of Health |
| IIR/IIR-M |
| 5.2.5.3 |
| A29R-14 |
| Clear SPU Error Flag |
| 20 |
| 2.27 Resolve Payload Subsystem Anomaly |
| IIA |
| 5.2.5.3 |
| A23-20 |
| Command SV Untrackable/Trackable |
| IIR/IIR-M |
| 5.2.6.1 |
| A23R-10 |
| Command SV Untrackable/Trackable |
| IIR/IIR-M |
| 5.2.9.1 |
| A25R-10 |
| SV Transmitting Extended L3 |
| 21 |
| 2.28 Resolve ITS Anomalous Commanding |
| IIA |
| 5.2.9.1 |
| A27-10 |
| ITS/RFDU Anomaly Resolution |
| IIR/IIR-M |
| 5.2.11.1 |
| A27R-10 |
| Commanded System Test |
| IIR/IIR-M |
| 5.2.11.2 |
| A27R-20 |
| ITS Telemetry Fails To Update |
| 22 |
| 2.29 Resolve LBD Anomalous Commanding |
| IIA |
| 5.2.8.1 |
| A26-10 |
| Switching To L1 or L2 HPA Backup |
| IIA |
| 5.2.8.4 |
| A26-40 |
| L3 Fails To Turn Off |
| IIR/IIR-M |
| 3.2.9.4 |
| R26R-10 |
| Configure L1/L2 |
| IIR/IIR-M |
| 3.2.9.6 |
| R26R-40 |
| Configure L3 Components |
| 23 |
| 3.11 Perform Navigation Upload Transmission Anomaly Procedures |
| IIA and IIR/IIR-M |
| 5.3.4.2 |
| A34-4 |
| Block IIA And IIR NAV Upload Transmission Anomaly |
| IIR/IIR-M |
| 5.3.4.2 |
| A34R-4 |
| Block IIR Navigation Upload Transmission Anomaly |
40 APPENDIX D: Payload Advanced Training Capabilities Table D-1: Payload Advanced Training Capabilities
| Ref No |
| PA Task |
| SV Model |
| SVMM Location |
| Checklist |
| Description |
| Additional Details |
| 1 |
| 1.7 Perform Monitor Station Anomaly Resolution |
| IIA and IIR/IIR-M |
| 5.3.5.1 |
| A35-1 |
| MS Initialization |
| IIA and IIR/IIR-M |
| 5.3.5.2 |
| A35-2 |
| MS Frequency Standard Switch |
| 2 |
| 2.9 Perform Timekeeping Ephemeris Actions |
| IIA and IIR/IIR-M |
| 3.3.7.1 |
| R36-51S |
| USNO Time Transfer Update |
| Easily operated in the GSF. Reference SVMM Section 2.1.2.8: USNO Download for further details. |
| 3 |
| 3.7 Perform Payload Upload Procedures |
| IIA and IIR/IIR-M |
| 3.3.4.6 |
| R33-61 |
| Routine Nav Upload |
| Difficult situation to create in GSF; essential fix action for anomaly. Checklist difficulty mandates it as an essential training task. |
| IIA |
| 3.3.4.9 |
| R33-64 |
| Crypto Variable Upload |
| IIR/IIR-M |
| 3.3.4.8 |
| R33-64 |
| Crypto Variable Upload |
| 4 |
| 3.14 Resolve General Payload Anomaly |
| IIA |
| 5.3.4.3 |
| A34-7 |
| Tracking Non Standard Code |
| IIR/IIR-M |
| 5.3.4.3 |
| A34R-7 |
| Tracking Non Standard Code |
| 5 |
| 3.9 Perform Payload Support Operations |
| IIA and IIR/IIR-M |
| 3.3.3.1 |
| R32-51 |
| Periodic HANU Messages |
| 6 |
| 3.12 Perform MCS Fix Actions |
| IIA and IIR/IIR-M |
| 5.3.2.3 |
| A32-2 |
| HANU Resolution |
| Reference SVMM Section 5.1.5: Upload Generation Failure for further details. |
| 7 |
| 3.20 Perform Kalman Filter Maintenance Operations |
| IIA and IIR/IIR-M |
| 3.3.4.1 |
| R33-51 |
| Momentum Dump Kalspoil |
| Have to Manually break the SVs in the GSF, need easier input. Helpful in performance of several anomalous fix actions, but less of a high priority than the other 3.20 tasks. |
| IIA and IIR/IIR-M |
| 3.3.4.5 |
| R33-58 |
| SV Partitioning |
| IIA and IIR/IIR-M |
| 5.3.3.1 |
| A33-3 |
| Clock Modify |
3.1 Perform Payload Display Checks
| IIA and IIR/IIR-M |
| 3.1.1.1 |
| CL3-1 |
| Crew Changeover (Nav System Check, Step 13) |
| IIA and IIR/IIR-M |
| 2.1.2.2 |
| N/A |
| Visibility Check |
| Reference SVMM Section 2.1.2.2: Visibility Check Guidance for further details. |
| 9 |
| 3.13 Perform Measurement Out of Tolerance Fix Actions |
| IIA |
| 5.3.3.3 |
| A33-6 |
| Failed Block IIA Pseudo Range Residuals (PRRs) |
| IIA and IIR/IIR-M |
| 5.3.3.4 |
| A33-7 |
| Ranging Errors Out of Tolerance |
| IIR/IIR-M |
| 5.3.3.3 |
| A33R-6 |
| Pseudo Range Residuals Out Of Tolerance |
3.16 Perform L-Band Anomaly
Navigation Data Errors
| IIA |
| 5.2.11.2 |
| N/A |
| Navigation Data Reference SVMM Section 5.2.11.2 Navigation Data Errors for further details |
| . |
| IIR/IIR-M |
| 5.2.12.2 |
| N/A |
| Reference SVMM Section 5.2.12.2 Navigation Data Errors for further details |
L-Band Lock Problems
| IIA |
| 5.2.11.3 |
| N/A |
| Reference SVMM Section 5.2.11.3: L-Band Lock Problems for further details |
| IIR/IIR-M |
| 5.2.12.3 |
| N/A |
| Reference SVMM Section 5.2.12.3: L-Band Lock Problems for further details |
L-Band Monitor Actions
| IIA |
| 5.2.11.4 |
| N/A |
| Reference SVMM Section 5.2.11.4: L-Band Monitor Problems for further details |
| IIR/IIR-M |
| 5.2.12.4 |
| N/A |
| Reference SVMM Section 5.2.12.4: L-Band Monitor Problems for further details |
| 11 |
| 3.8 Perform Nominal Payload Procedures |
| IIA and IIR/IIR-M |
| 3.3.4.2 |
| R33-52 |
| Reference File Update |
| IIA and IIR/IIR-M |
| 3.3.4.4 |
| R33-56 |
| Almanac Generation / Update |
| IIA and IIR/IIR-M |
| 5.3.3.5 |
| A33-8 |
| Linearity Test Failure Verification |
| IIA and IIR/IIR-M |
| 3.3.8.2 |
| R37-52 |
| 90 Day Clock Forecast |
| 12 |
| 3.19 Perform User Notification Change Procedures |
| IIA |
| 3.3.4.8 |
| R33-63 |
| Special Messages |
| IIR/IIR-M |
| 3.3.4.7 |
| R33-63 |
| Special Messages |
| IIA and IIR/IIR-M |
| 5.3.3.2 |
| A33-5 |
| SV Health Status |
| IIA and IIR/IIR-M |
| 5.3.2.2 |
| A32-1 |
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