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CAGE CODE
| NUMBER |
| REVISION |
| DATE |
| PAGE |
| 2D605 |
| SS-PTE-615 |
| B |
| 09 Sept 2009 |
| ii |
Document Revision & Version History
| Document |
| Revision |
| Date |
| Event |
| SS-PTE-615 |
| New |
| 12 March 2009 |
| Initial Release |
| SS-PTE-615 |
| A |
Renumber Requirement IDs to Sections 3, 5 and Appendix A
| SS-PTE-615 |
| B |
| 09 Sept 2009 |
| Added updates for V5.5 |
TBD ITEMS
| Section |
| Item TBD |
| Resolution Date |
| None |
| None |
| None |
Table of Contents
11 SCOPE
11.1 Identification
11.2 System Overview
11.2.1 Global Positioning System
11.2.2 PTE Mission
11.2.3 History
21.2.4 Organization and Support Agencies
21.2.5 PTE Operations
21.3 Document Overview.
21.3.1 Document Requirements Terminology and Use
32 REFERENCED DOCUMENTS
32.1 Government Documents
32.2 Referenced Documents
43 REQUIREMENTS
43.1 States and Modes
43.2 Infrastructure
43.2.1 General
84 QUALIFICATION PROVISIONS
84.1 Test Program
84.1.1 Verification Method
94.2 Verification Methods
94.2.1 Demonstration
94.2.2 Test
94.2.3 Analysis
94.2.4 Inspection
105 REQUIREMENTS TRACEABILITY
136 NOTES
136.1 Acronyms
Appendix A Requirements Verification A-
List of Tables
10Table 5-1: Requirements Traceability Matrix
1 SCOPE
1.1 Identification
This Prime Item Development Specification (PIDS), SS-PTE-615, specifies the requirements and qualification provisions for the Global Positioning System (GPS) Positional Training Emulator (PTE). 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 (STAR Sim), and Instructor Control (IC).
1.2 System Overview
1.2.1 Global Positioning System
The GPS consists of three segments: the Space Segment, the Control Segment, and the User Segment. The Space Segment currently consists of IIA, IIR and IIF space vehicle block types. Within the control segment, the OCS consists of the AEP (command & control), the Ground Antenna(s) and the Monitor Stations. PTE trains GPS crews how to operate the entire space segment and the OCS.
1.2.2 PTE Mission
The mission of the PTE is to provide a realistic training environment that supports crew training and positional training for the Global Positioning System Operational Control System operators.
PTE provides a GPS training capability for Basic Operator (BOPR) Training and Advanced Operator Training that includes Vehicle Advanced, Payload Advanced, Crew Advanced and Navigation Warfare (NAVWAR) training.
1.2.3 History
The Air Force has an urgent requirement to train operational personnel on the new GPS AEP OCS currently being developed by Boeing. In conjunction with this effort, the Air Force has requested development of a Positional Training Emulator (PTE), which can provide a crew and positional training capability for the GPS Space Segment (SS) and OCS. Boeing will deliver the PTE in a classified software/ hardware configuration, which retains the training capabilities inherent in the AEP/GPS Simulator (GPSS) combination and adds capabilities specific to positional training and instructor control.
The need to develop an AEP PTE is documented in a memorandum, dated 21 November 2006, from the 50th Operations Group.
1.2.4 Organization and Support Agencies
The GPS Space Wing manages the GPS program. The program director is delegated the authority to develop, coordinate, and direct the GPS program. The Global Positioning System Wing (GPSW) develops and maintains the GPS, including the PTE..
1.2.5 PTE Operations
Air Force Space Command (AFSPC) is the PTE Operations Agency and all operating facilities within the PTE system are under the control and direction of AFSPC.
1.3 Document Overview.
The purpose of this document 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 and hardware linking the requirements specified in this element level specification, notes, and 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
The following documents, for the issues shown, form a part of this specification to the extent specified herein. In the event of conflict between the documents referenced herein and the contents of this specification, the contents of this specification supersede the contents of the referenced documents.
2.2 Referenced Documents
| SS-CS-600 Rev D |
| Segment Specification for the Block IIF NAVSTAR Global Positioning System Control Segment |
3 REQUIREMENTS
3.1 States and Modes
| SS-PTE-34 |
| 3.1.1 There are effectively two states for the PTE: Scenario Preparation and Scenario Execution. Within the Execution state the PTE shall operate in two modes: Crew or Positional. |
| SS-PTE-35 |
| 3.1.2 In the Crew mode the PTE shall support the following positions simultaneously: Satellite System Operator (SSO), Space Vehicle Operator (SVO), Payload System Operator (PSO), Mission Commander (MC), Mission Chief (MCH) and Navigation Warfare Officer (NWO). |
| SS-PTE-36 |
| 3.1.3 In the Positional mode the PTE shall support the configuration of initial conditions to support multiple independent student training. |
| SS-PTE-37 |
| 3.1.4 In the Positional mode the PTE shall allow all students scenario to function independently without interaction or interference from other student’s activities. |
| SS-PTE-38 |
| 3.1.5 In the Positional mode the PTE shall allow all students within a training session to train on the same task (performance worksheet), work independently and progress at their own pace. |
| SS-PTE-39 |
| 3.1.6 Independent control of each student’s scenario shall be made available to the instructor. |
3.2 Infrastructure
3.2.1 General
| SS-PTE-43 |
| 3.2.1.1 Hardware |
PTE shall use a consolidated hardware architecture able to run AEP, SIM, and IC software with no external interface connectivity.
| SS-PTE-44 |
| 3.2.1.2 PTE shall execute on a single instance of an Master Control Station (MCS) hardware suite in a consolidated server configuration. |
The PTE MCS hardware suite does not include the following components found in the operational MCS:
· Crypto servers
· Server redundancy (no failover capability)
· Mission Operations Transfer (MOX) hardware suite
· Almanac PC
· SBMCS PC
| SS-PTE-51 |
| 3.2.1.3 PTE shall support 10 Consolidated Operator Support Environment (COSE) workstations each configured with three display monitors. |
| SS-PTE-52 |
| 3.2.1.4 PTE shall provide Julian-date and time display hardware to provide the simulation time for the training scenario. |
| SS-PTE-54 |
| 3.2.2 Capability Baseline |
PTE shall provide a training system that incorporates baseline AEP and Global Positioning System Simulator (GSS) software.
| SS-PTE-56 |
| 3.2.3 Single Universe |
PTE shall provide a single universe for all student sessions consisting of a single constellation of GPS satellites with S-Band and L-Band ground stations.
| SS-PTE-58 |
| 3.2.4 Advanced Positional Training |
PTE shall provide a positional training system that can be used for training tasks for the SSO,SVO,PSO, MC, MCH and NWO positions.
| SS-PTE-60 |
| 3.2.5 Crew Training |
PTE shall support crew training for up to six different crew positions.
| SS-PTE-62 |
| 3.2.6 Displays and Indicators |
PTE shall allow students to be able to determine the functional status from displays and indicators and individually interact with instructor assigned scenarios.
3.2.7 Training Features
| SS-PTE-65 |
| 3.2.7.1 Control Anomalies |
PTE shall permit the instructor to inject anomalies (SV, ground station).
| SS-PTE-67 |
| 3.2.7.2 Scenario Scripts Creation |
PTE shall permit the instructor to create and modify scenario scripts.
| SS-PTE-69 |
| 3.2.7.3 Training Scenarios |
PTE shall permit the instructor to create and modify training scenarios.
| SS-PTE-71 |
| 3.2.7.4 Scenario Script Execution |
PTE shall permit the instructor to execute scenario scripts.
| SS-PTE-73 |
| 3.2.7.5 Student Monitoring |
PTE shall permit the instructor to monitor student displays.
| SS-PTE-75 |
| 3.2.7.6 Startup/Shutdown |
PTE shall permit the instructor to control Startup and Shutdown.
| SS-PTE-77 |
| 3.2.7.7 Scenario Initial Conditions |
PTE shall permit configuration of scenario initial conditions to support multiple independent student training.
| SS-PTE-79 |
| 3.2.7.8 Pause/Resume |
PTE shall permit pause and resume operation.
| SS-PTE-81 |
| 3.2.7.9 Fast/Slow |
PTE shall permit fast and slow forward operations.
| SS-PTE-83 |
| 3.2.7.10 Save/Restore |
PTE shall permit state save and restore operations.
| SS-PTE-85 |
| 3.2.7.11 Logging |
PTE shall permit logging of student activities.
3.2.8 Operator Training
| SS-PTE-88 |
| 3.2.8.1 BOPR Training |
PTE shall provide a positional training system that can be used for BOPR training tasks for up to 10 SSO students simultaneously.
| SS-PTE-90 |
| 3.2.8.2 Vehicle Advanced Training |
PTE shall provide a positional training system that can be used for Vehicle Advanced training tasks for up to 10 SVO students simultaneously.
| SS-PTE-92 |
| 3.2.8.3 Payload Advanced Training |
PTE shall provide a positional training system that can be used for Payload Advanced training tasks for up to 10 PSO students simultaneously..
| SS-PTE-94 |
| 3.2.8.4 Crew Advanced Training |
PTE shall provide a positional training system that can be used for Crew Advanced training tasks for up to 10 MC/MCH students simultaneously.
| SS-PTE-243 |
| 3.2.8.5 NAVWAR Training |
PTE shall provide a positional training system that can be used for NWO training tasks for up to 10 NWO students simultaneously.
4 QUALIFICATION PROVISIONS
4.1 Test Program
For PTE, a Formal Qualification Test (FQT) event will not be performed as part of the rapid prototype process. Instead, demonstrations of the capabilities are performed with Air Force participation.
Formal test procedures will not be designed and generated. Instead, the Air Force training scenarios are used in place of test procedures. Since the training scenarios are essentially the GPS operating procedures, and the operating procedures have already been approved, there is no need to peer-review and re-approve the training scenarios for use in the verification demonstrations. Therefore, the verification method for requirements in this document (Appendix A) will be verified through demonstration.
Exception: Test procedures or scripts shall be used to demonstrate the set of Instructor Capabilities.
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 both the 50th Operational Support Squadron (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.
4.1.1 Verification Method
The contractor's test program will qualify each requirement in Appendix A.
4.2 Verification Methods
4.2.1 Demonstration
Demonstration 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
Test 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
Analysis 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
Inspection is the visual examination of system components, documentation, etc.
5 REQUIREMENTS TRACEABILITY
Table 5-1: Requirements Traceability Matrix
| Object Identifier |
| Paragraph ID |
| New Para Heading Only |
| SS-CS-600 Reqmt ID |
| SS-CS-600 Paragraph No. |
| SS-PTE-34 |
| 3.1.1 |
| States and Modes |
| N/A |
| N/A |
| SS-PTE-35 |
| 3.1.2 |
| States and Modes |
| N/A |
| N/A |
| SS-PTE-36 |
| 3.1.3 |
| States and Modes |
| N/A |
| N/A |
| SS-PTE-37 |
| 3.1.4 |
| States and Modes |
| N/A |
| N/A |
| SS-PTE-38 |
| 3.1.5 |
| States and Modes |
| N/A |
| N/A |
| SS-PTE-39 |
| 3.1.6 |
| States and Modes |
| N/A |
| N/A |
| SS-PTE-43 |
| 3.2.1.1 |
| Hardware |
| N/A |
| N/A |
| SS-PTE-44 |
| 3.2.1.2 |
| Hardware |
| N/A |
| N/A |
| SS-PTE-51 |
| 3.2.1.3 |
| Hardware |
| N/A |
| N/A |
| SS-PTE-52 |
| 3.2.1.4 |
| Hardware |
| N/A |
| N/A |
| SS-PTE-54 |
| 3.2.2 |
| Capability Baseline |
| N/A |
| N/A |
| SS-PTE-56 |
| 3.2.3 |
| Single Universe |
| N/A |
| N/A |
| SS-PTE-58 |
| 3.2.4 |
| Advanced Positional Training |
| N/A |
| N/A |
| SS-PTE-60 |
| 3.2.5 |
| Crew Training |
| N/A |
| N/A |
| SS-PTE-62 |
| 3.2.6 |
| Displays and Indicators |
| N/A |
| N/A |
| SS-PTE-65 |
| 3.2.7.1 |
| Control Anomalies |
| N/A |
| N/A |
| SS-PTE-67 |
| 3.2.7.2 |
| Scenario Scripts Creation |
| N/A |
| N/A |
| SS-PTE-69 |
| 3.2.7.3 |
| Training Scenarios |
| N/A |
| N/A |
| SS-PTE-71 |
| 3.2.7.4 |
| Scenario Script Execution |
| N/A |
| N/A |
| SS-PTE-73 |
| 3.2.7.5 |
| Student Monitoring |
| N/A |
| N/A |
| SS-PTE-75 |
| 3.2.7.6 |
| Startup/Shutdown |
| N/A |
| N/A |
| SS-PTE-77 |
| 3.2.7.7 |
| Scenario Initial Conditions |
| N/A |
| N/A |
| SS-PTE-79 |
| 3.2.7.8 |
| Pause/Resume |
| N/A |
| N/A |
| SS-PTE-81 |
| 3.2.7.9 |
| Fast/Slow |
| N/A |
| N/A |
| SS-PTE-83 |
| 3.2.7.10 |
| Save/Restore |
| N/A |
| N/A |
| SS-PTE-85 |
| 3.2.7.11 |
| Logging |
| N/A |
| N/A |
| SS-PTE-88 |
| 3.2.8.1 |
| BOPR Training |
| N/A |
| N/A |
| SS-PTE-90 |
| 3.2.8.2 |
| Vehicle Advanced Training |
| N/A |
| N/A |
| SS-PTE-92 |
| 3.2.8.3 |
| Payload Advanced Training |
| N/A |
| N/A |
| SS-PTE-94 |
| 3.2.8.4 |
| Crew Advanced Training |
| N/A |
| N/A |
| SS-PTE-243 |
| 3.2.8.5 |
| NAVWAR Training |
| N/A |
| N/A |
6 NOTES
6.1 Acronyms
| AEP |
| Architecture Evolution Program |
| AFSCN |
| Air Force Satellite Control Network |
| AFSPC |
| Air Force Space Command |
| BOPR |
| Basic Operator |
| COSE |
| Consolidated Operator Support Environment |
| FQT |
| Formal Qualification Test |
| GFE |
| Government Furnished Equipment |
| GFP |
| Government Furnished Property |
| GPS |
| Global Positioning System |
| GPSW |
| Global Positioning System Wing |
| GSS |
| Global Positioning System Simulator |
| IAW |
| In Accordance With |
| IC |
| Instructor Control |
| ICD |
| Interface Control Document |
| II/IIA |
| GPS Block II/IIA Space Vehicle |
| IIF |
| GPS Block IIF Space Vehicle |
| IIR |
| GPS Block IIR Space Vehicle |
| LADO |
| Launch/early orbit, Anomaly resolution, and Disposal Operations |
| MC |
| Mission Commander |
| MCH |
| Mission Chief |
| MCS |
| Master Control Station |
| MOX |
| Mission Operations Transfer |
| NAVWAR |
| Navigation Warfare |
| NWO |
| Navigation Warfare Officer |
| OCS |
| Operational Control System |
| OSS |
| Operational Support Squadron |
| PAO |
| Payload Advanced Operator |
| PC |
| Personal Computer |
| PIDS |
| Prime Item Development Specification |
| PSO |
| Payload System Operator |
| PTE |
| Positional Training Emulator |
| QA |
| Quality Assurance |
| SAFB |
| Schriever Air Force Base |
| SBMCS |
| Space Battle Management Master Control Station |
| SIM |
| Simulator |
| SS |
| Space Segment |
| SSO |
| Satellite System Operator |
| STAR Sim |
| Satellite Training and Rehearsal Simulator |
| SV |
| Space Vehicle |
| SVO |
| Space Vehicle Operator |
| TBD |
| To Be Determined |
| VCRM |
| Verification Cross Reference Matrix |
| VS |
| Verification Sheets |
7 Appendix A Requirements Verification
| Object Identifier |
| New Para |
| A |
| D |
| I |
| T |
| SS-PTE-34 |
| 3.2.1.1 States and Modes |
X
| SS-PTE-35 |
| 3.2.1.2 States and Modes |
X
| SS-PTE-36 |
| 3.2.1.3 States and Modes |
X
| SS-PTE-37 |
| 3.2.1.4 States and Modes |
X
| SS-PTE-38 |
| 3.2.1.5 States and Modes |
X
| SS-PTE-39 |
| 3.2.1.6 States and Modes |
X
| SS-PTE-43 |
| 3.2.1.1 Hardware |
X
| SS-PTE-44 |
| 3.2.1.2 Hardware |
X
| SS-PTE-51 |
| 3.2.1.3 Hardware |
X
| SS-PTE-52 |
| 3.2.1.4 Hardware |
X
| SS-PTE-54 |
| 3.2.2 Capability Baseline |
X
| SS-PTE-56 |
| 3.2.3 Single Universe |
X
| SS-PTE-58 |
| 3.2.4 Advanced Positional Training |
X
| SS-PTE-60 |
| 3.2.5 Crew Training |
X
| SS-PTE-62 |
| 3.2.6 Displays and Indicators |
X
| SS-PTE-65 |
| 3.2.7.1 Control Anomalies |
X
| SS-PTE-67 |
| 3.2.7.2 Scenario Scripts Creation |
X
| SS-PTE-69 |
| 3.2.7.3 Training Scenarios |
X
| SS-PTE-71 |
| 3.2.7.4 Scenario Script Execution |
X
| SS-PTE-73 |
| 3.2.7.5 Student Monitoring |
X
| SS-PTE-75 |
| 3.2.7.6 Startup/Shutdown |
X
| SS-PTE-77 |
| 3.2.7.7 Scenario Initial Conditions |
X
| SS-PTE-79 |
| 3.2.7.8 Pause/Resume |
X
| SS-PTE-81 |
| 3.2.7.9 Fast/Slow |
X
| SS-PTE-83 |
| 3.2.7.10 Save/Restore |
X
| SS-PTE-85 |
| 3.2.7.11 Logging |
X
| SS-PTE-88 |
| 3.2.8.1 BOPR Training |
X
| SS-PTE-90 |
| 3.2.8.2 Vehicle Advanced Training |
X
| SS-PTE-92 |
| 3.2.8.3 Payload Advanced Training |
X
| SS-PTE-94 |
| 3.2.8.4 Crew Advanced Training |
X
| SS-PTE-243 |
| NAVWAR Training |
X
� EMBED Word.Document.8 \s ���
Officially Released
09 July 2009
Signatures on File
Officially Released
27 October 2009
Signatures on File i
_1318139551.doc
PREPARED BY
CAGE CODE 2D605
NUMBER
REVISION
Larry Oshiro
SS-PTE-615
B
The Boeing Company
TYPE
APPROVALS
ENGINEERING
AUTHORITY
CS SEIT –
Ryan Witham
WBS 440
PRIME ITEM DEVELOPMENT SPECIFICATION
DATE
9/9/09
TOTAL PAGES
SUBJECT:
EFFECT ON RELEASE TO FILES
CHANGE/RELEASE
PSDR/NR
PRIME ITEM DEVELOPMENT SPECIFICATION
FOR THE
POSITIONAL TRAINING EMULATOR
OF THE
GLOBAL POSITIONING SYSTEM BLOCK IIF
CONTRACT NO. F04701-96-C-0025
ADPL SEQUENCE NO. ADP 102-B
Prepared for:
U.S. AIR FORCE
HEADQUARTERS SPACE & MISSILE SYSTEMS CENTER
LOS ANGELES, CA 90009-2960
Prepared by:
The Boeing Company
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.
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