Cospas-Sarsat specification summaries moved to reference/ for internal use only. Links updated to point to official cospas-sarsat.int site. The extracted images remain in public/ for use in other pages.
591 lines
35 KiB
Markdown
591 lines
35 KiB
Markdown
---
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title: "R017: C/S R.017 - Issue 1 Rev. 7"
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description: "Official Cospas-Sarsat R-series document R017"
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sidebar:
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badge:
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text: "R"
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variant: "note"
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# Extended Cospas-Sarsat metadata
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documentId: "R017"
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series: "R"
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seriesName: "Reports"
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documentType: "report"
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isLatest: true
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issue: 1
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revision: 7
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documentDate: "March 2021"
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originalTitle: "C/S R.017 - Issue 1 Rev. 7"
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---
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> **📋 Document Information**
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>
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> **Series:** R-Series (Reports)
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> **Version:** Issue 1 - Revision 7
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> **Date:** March 2021
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> **Source:** [Cospas-Sarsat Official Documents](https://www.cospas-sarsat.int/en/documents-pro/system-documents)
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---
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SECOND GENERATION
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406 MHz BEACON IMPLEMENTATION PLAN
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C/S R.017
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Issue 1 - Revision 7
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SECOND GENERATION
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406 MHz BEACON IMPLEMENTATION PLAN
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History
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Issue
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Revision
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Date
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Comments
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Approved by the Cospas-Sarsat Council (CSC-47)
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Approved by the Cospas-Sarsat Council (CSC-49)
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Approved by the Cospas-Sarsat Council (CSC-51)
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Approved by the Cospas-Sarsat Council (CSC-53)
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Approved by the Cospas-Sarsat Council (CSC-55)
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Approved by the Cospas-Sarsat Council (CSC-56)
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Approved by the Cospas-Sarsat Council (CSC-57)
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Approved by the Cospas-Sarsat Council (CSC-64)
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TABLE OF CONTENTS
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Page
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History ................................................................................................................................................. i
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Table of Contents ................................................................................................................................. ii
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1.
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INTRODUCTION .............................................................................................. 1-1
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1.1
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Purpose of the Document ..................................................................................... 1-1
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1.2
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Background .......................................................................................................... 1-1
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1.3
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Goals 1-2
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2.
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ASSUMPTIONS AND CONSTRAINTS ......................................................... 2-1
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2.1
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Assumptions ......................................................................................................... 2-1
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2.2
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Constraints ............................................................................................................ 2-1
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3.
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IMPLEMENTATION ACTIVITIES AND TIME LINE ............................... 3-1
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3.1
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Second Generation Beacon Definition and Development Phase ......................... 3-3
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3.1.1 Development of Operational Requirements ............................................. 3-3
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3.1.2 Preliminary Technical Evaluation and Main System Definition and Trade-
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offs ............................................................................................................ 3-4
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3.1.3 Final Technical Assessment and Refined System Trade-offs .................. 3-4
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3.1.4 Development of Second Generation Beacon Specification Document
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(C/S T.018) ............................................................................................... 3-4
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3.1.5 Development of Second Generation Compatible LUT Specifications ..... 3-5
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3.2
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Proof of Concept Phase ........................................................................................ 3-5
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3.2.1 Proof of Concept Testing.......................................................................... 3-6
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3.2.2 Modifications of other Relevant Cospas-Sarsat Documents .................... 3-6
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3.2.3 Development of SGB Type Approval Standards and Acceptance of
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Test Facilities ........................................................................................... 3-7
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3.3
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Transition to Operations Phase ............................................................................ 3-7
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3.3.1 Documentation Revisions and Finalizations ............................................ 3-7
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3.3.2 Second Generation LUT Commissioning Standards ................................ 3-7
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3.3.3 Second Generation Beacon and Second Generation Ground Segment
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System Testing ......................................................................................... 3-8
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3.3.4 Test Facilities Prepare for SGB Type Approval Tests ............................. 3-8
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3.3.5 Re-acceptance of Type Approval Test Facilities for SGB Type Approval
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Tests .......................................................................................................... 3-8
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3.4
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SGB Transition Phase .......................................................................................... 3-9
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3.5
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MEOSAR Global Coverage - Encoded Locations (To Accommodate SGB
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ELT(DTs)) ............................................................................................. 3-9
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3.6
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SGB Full Operational Capability (FOC) ............................................................ 3-10
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3.6.1 Type Approval of Second Generation Beacons ..................................... 3-10
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3.6.2 Updates to National and International Standards ................................... 3-10
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1-1
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1.
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INTRODUCTION
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1.1
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Purpose of the Document
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This plan addresses the development and deployment of second generation 406 MHz beacons into
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the Cospas-Sarsat System.
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The plan describes high level tasks and activities expected to be undertaken by Cospas-Sarsat
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Participants and other stakeholders to ensure the effective development, production and
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introduction to the market of second generation 406 MHz beacons. The plan also provides tentative
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time lines for the various tasks required for second generation beacon implementation along with
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a brief description of the required inputs and expected outputs associated with each task.
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This plan also describes the higher level tasks and activities needed to use the SGB signal to meet
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the ICAO GADSS requirements for an ELT(DT).
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1.2
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Background
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The International Cospas-Sarsat System has been successfully operating since 1982 and has
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achieved world-wide recognition as a provider of satellite distress alerts to search and rescue
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(SAR) authorities. The carriage of Cospas-Sarsat 406 MHz distress beacons, whether mandated
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by Administrations 1or as a result of voluntary use by individuals at risk, is becoming increasingly
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popular.
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The LEOSAR and GEOSAR systems comprise the current operational Space Segment. Cospas-
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Sarsat is developing a new satellite alerting capability, the MEOSAR system, which is expected
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to replace the LEOSAR system. The MEOSAR system is planned to begin operating in the 2012
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- 2015 time frame and become fully operational during the second half of the decade. The
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MEOSAR system will be backward compatible and will accommodate the operation of first-
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generation Cospas Sarsat beacons as specified in document C/S T.001. The MEOSAR system is
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also expected to provide enhanced performance for all 406 MHz beacons currently in operation,
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to include global, near instantaneous alerting and locating capabilities and greater resilience to
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beacon-to-satellite obstructions. Detailed information on MEOSAR system development is
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available in the document C/S R.012 "Cospas-Sarsat 406 MHz MEOSAR Implementation Plan".
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1 On board aircraft and ships is mandated by Administrations in accordance with the recommendations of the
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International Civil Aviation Organization (ICAO) and the International Maritime Organization (IMO). Their use on
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board fishing vessels, pleasure craft and general aviation aircraft is also a requirement in numerous countries.
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1-2
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The MEOSAR system uses a time/frequency measurement to compute the position of a distress
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beacon. It also allows for a return link to the beacon. Preliminary analyses have indicated that a
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new generation of 406 MHz beacon designed to operate in a MEOSAR environment could further
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enhance the performance of the Cospas-Sarsat system in the future.
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1.3
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Goals
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The deployment of second generation 406 MHz beacons requires that a number of tasks and
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activities be accomplished and coordinated among various Cospas-Sarsat stakeholders. The
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second generation 406 MHz beacon implementation plan allows the Cospas-Sarsat Programme to:
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a) plan for updated beacon standards to reflect the agreed second generation beacon
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operational requirements described in Cospas-Sarsat document C/S G.008;
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b) outline of activities needed to successfully complete the implementation of a second
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generation of distress beacons; and
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c) provide a time line for second generation beacon implementation.
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The second generation 406 MHz beacon implementation plan is managed by the Cospas Sarsat
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Council which will coordinate its implementation with other stakeholders involved in the
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development of future 406 MHz distress beacons.
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- END OF SECTION 1 -
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2-1
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2.
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ASSUMPTIONS AND CONSTRAINTS
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2.1
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Assumptions
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First generation beacon specifications documented in C/S T.001 were derived from technical
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characteristics optimized for the LEOSAR system. This system uses frequency shift measurements
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of 406 MHz transmissions during periodic passage of satellite payloads at low elevation angles for
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independent location determination.
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Second generation beacon specifications will be developed assuming operation with the Cospas-
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Sarsat GEOSAR and MEOSAR systems comprised only of Search and Rescue Repeaters (SARR)
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instruments and with all signal and data processing performed by ground receiving stations called
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Local User Terminals or LUTs. A MEOSAR FOC System will be available to provide the alerting
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and locating functions on a global basis. Independent position determination will be established
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based on trilateration using the time and frequency of arrival (TOA and FOA) measurements of
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the signals received from distress beacons. The methodology involves the processing by
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MEOLUTs of signals received from multiple payloads distributed around the beacon at various
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elevation angles. The determination of the optimal characteristics required from second generation
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beacon to operate within this new environment will need to consider possible trade-off between
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the expected performances of the various segment of the system.
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2.2
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Constraints
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The current GEOSAR space segment is in operation and the planned MEOSAR space segment has
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already been designed. Specifications for second generation beacons will be constrained by the
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characteristics of these constellations and the design of their Search and Rescue instruments.
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The GEOSAR and MEOSAR constellations will consist of various satellite systems which could
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introduce variations of performance levels due to system design differences. Minimum interface
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requirements have been established to minimise such variations and ensure full interoperability
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with commissioned space and ground segment equipment in the Cospas Sarsat System. These
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requirements are constraints to be taken into consideration in the cost and benefit trade offs for the
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development of second generation beacon specifications.
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In order to maintain the relevance of 406 MHz beacons, second generation beacon specifications
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should allow for technology to be available at a reasonable cost to users.
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Second generation beacons designed to meet new specifications may not be interoperable with the
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LEOSAR SARP processing. If second generation beacons are not interoperable with LEOSAR
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SARP instruments, the LEOSAR system will not provide the alerting and locating functions for
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these beacons on a global basis.
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2-2
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Modifications to beacon signal characteristics and coding protocols will require new processing
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software to be implemented in existing GEOLUTs to provide the alerting service. Additionally,
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MEOLUTs installed by Participants to support the MEOSAR system development may require
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upgrades to be compatible with second generation beacons. Furthermore, in regions where
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MEOLUT coverage will not be adequate prior to the MEOSAR FOC, existing LEOLUTs may
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also need to be upgraded to process second generation beacon signals relayed via LEOSAR
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satellite repeaters (SARR).
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A MEOSAR FOC System will be necessary in order to provide the alerting and locating functions
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on a global basis.
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Finally, software upgrades will also be implemented in Cospas-Sarsat Mission Control Centres
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(MCCs) to forward and distribute distress alerts originating from second generation beacons to
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Rescue Coordination Centres (RCCs) and SAR Points of Contact (SPOCs).
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The time line of second generation beacon deployment activities will need to take in consideration
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all of these constraints.
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- END OF SECTION 2 -
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3-1
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3.
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IMPLEMENTATION ACTIVITIES AND TIME LINE
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This section establishes a timeline of the different phases, tasks and milestones that will lead to
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introduction of SGBs into the Cospas-Sarsat System. The timeline of each event is based upon
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reasonable assumptions of the work required, and a linear flow of each stage of development.
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Figure 1 provides a list of high level tasks expected to be completed for the deployment of second
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generation beacons, along with a tentative time line for each tasks. The schedule also includes
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major Cospas-Sarsat meetings where relevant documents and progress reports will be reviewed.
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The following sections provide a brief explanation of the activities required for the deployment of
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second generation beacons along with the inputs expected to trigger the activities and their
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expected output.
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3-2
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Figure 1: Second Generation Beacon Implementation Schedule
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Figure 1 Notes:
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\#1 [SGL] refers to MEOLUTs and GEOLUTs that are capable of processing Second Generation Beacons.
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\#2 The target date for completeion of this activity is JC-35. However, this activity may require the extension to an
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EWG as convened by the Council between JC-35 and CSC-65 or CSC-66.
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3-3
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3.1
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Second Generation Beacon Definition and Development Phase
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During this phase Cospas-Sarsat will focus on determining operational requirements for
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second generation beacons and compatibility with existing Cospas-Sarsat System components.
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Systems analysis and design will then be performed to determine the optimal implementation
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method to meet these requirements. The required beacon characteristics will be documented in a
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new beacon specification (document C/S T.018). This document will be used by beacon
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manufacturers to develop new beacon models. These documents will continue to be developed and
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refined during the Proof of Concept phase. In parallel with this development, it is expected that
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other Cospas-Sarsat specifications will be updated, such as G.005 (Cospas-Sarsat Guidelines on
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406 MHz Beacon Coding, Registration and Type Approval), T.012 (Cospas-Sarsat 406 MHz
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Frequency Management Plan), and T.014 (Cospas-Sarsat Frequency Requirements and
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Coordination Procedures).
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3.1.1
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Development of Operational Requirements
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This task is the initial step for the development of relevant second generation beacon specifications
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and consists in the generation of minimum and objective operational requirements expected to be
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met by second generation beacons operating in the Cospas Sarsat MEOSAR System. The task
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involves the participation of various Cospas Sarsat stakeholders, in particular Search and Rescue
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(SAR) organizations which will use the information provided by the SGBs. The outcome of this
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activity is compiled in document C/S G.008 "Operational Requirements for Cospas-Sarsat
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406 MHz beacons".
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This activity is completed when document C/S G.008 is approved by the Cospas Sarsat Council.
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However, the document may need to be reviewed and updated in the future, in particular once the
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technical evaluation of the requirements has been completed.
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Although some operational requirements could be challenging to attain, especially during the
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initial phase of the MEOSAR system implementation programme, it is expected that these
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requirements will stimulate innovation and be achieved in the long-term.
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3.1.1.1 Operational Requirements Matrix
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The development of operational requirements has yielded a detailed list of beacon requirements.
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These requirements must be met by either the beacon, the Space Segment, the LUTs, the MCCs,
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or through a collaborative effort of any combination of the various segments. Every segment is
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involved in achieving the final system design which will meet all of the operational requirements.
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Additionally, the space segment (SARR repeater) is already specified so it is excluded from the
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matrix.
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For a more beneficial requirements matrix, only the primary subsystems that are involved with
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meeting the operational requirements will be listed. For instance, the LUT must properly decode
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all information in the beacon message content; however, the primary subsystems involved in
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meeting the operational requirements for beacon message content will be the beacon and the MCC.
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3-4
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3.1.2
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Preliminary Technical Evaluation and Main System Definition and Trade-offs
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This task is initiated once beacon operational requirements are available. The core of this task
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consists in the performance evaluation and feasibility review of possible second generation beacon
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designs. The activity includes system trade-offs between expected performances of MEOSAR
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system, the operational LEOSAR and GEOSAR systems and SGB beacons, to address specific
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operational requirements, and should allow Cospas-Sarsat Participants to make decisions on the
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definition of second generation beacon designs and message structure.
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The completion of this task will finalise key signal design parameters and interoperability
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requirements of second generation beacons. It will also define message content and priority of
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information.
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3.1.3
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Final Technical Assessment and Refined System Trade-offs
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During this phase, the main beacon characteristics will be defined so that the development of the
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specifications and type approval standards can be finalized. If the beacons specifications deviate
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from the operational requirements due to a technical or cost trade off these would be identified.
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Recognizing that parallel approaches on beacon modulation scheme may be pursued (i.e., two
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different beacon designs) the comparison between approaches should be identified for evaluation
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by the Council. Other aspects of beacon design may be shared regardless of beacon modulation
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path taken. For example, beacon message content and homing requirements may be defined for
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both prospective paths.
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At a minimum, the Final Technical Assessment phase should yield the beacon specifications
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(C/S T.018) necessary to meet or exceed the operational requirements defined in document
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C/S G.008 or identify how and why there is a deviation from those requirements.
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3.1.4
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Development of Second Generation Beacon Specification Document(C/S T.018)
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This task is at the centre of the future second generation 406 MHz beacon development. This task
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will be done throughout the preliminary and final technical evaluation phases. The task consists of
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defining and creating second generation 406 MHz beacon specification document (C/S T.018).
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Since parallel beacon modulation schemes may be developed, two versions of the T.018 should be
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developed for each path to allow each approach to proceed independently.
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The changes in second generation beacon design and the added capabilities of these beacons will
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necessitate changes in the Cospas-Sarsat Type Approval Standard of 406 MHz beacons and Local
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User Terminal and Mission Control Centre specifications. These documents will need to be
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updated in later phases of development after further testing and evaluation of the SGB
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specifications.
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This task will be completed when the SGB specifications have been accepted by Council.
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3-5
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3.1.5
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Development of Second Generation Compatible LUT Specifications
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The changes to the LUTs in order to process the SGBs require new versions of specifications and
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commissioning standards to be developed for LUTS. The development of Second Generation
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Beacon Compatible LUT ([SGL]) critical task will begin near the end of the SGB Definition and
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Development phase and modified based on the results of the Proof of Concept (POC) Phase. The
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task will consist of developing the specifications for the LUT segments that are to be fully capable
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of processing transmissions from the SGBs. These specifications, analysed with the SGB
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specifications, should enable the operational requirements of G.008 to be met.
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Additionally, SGBs designed to T.018 specifications may not be interoperable with the LEOSAR
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SARP processing which may prevent these beacons from being located if coverage of [SGL]s is
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insufficient at that time.
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In particular providing global coverage for SGBs may require that:
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a) existing GEOLUTs be upgraded to process second generation beacon signals relayed via
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GEOSAR repeaters (SARR);
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b) MEOLUTs be designed or upgraded to process second generation beacon design signals
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relayed via MEOSAR repeaters; and
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c) LEOLUTs updated to make use of real time SARR data.
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Modifications to operational LUTs should only begin after [SGL] specifications have been
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developed. Developmental LUTs capable of processing T.018 transmissions could be developed
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at any time to allow for testing of SGB. Depending on the SGB design, developmental LUTs that
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are going to be relied upon to provide global coverage for SGBs must be available for POC and
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System SGB testing. For example if the SGB design relies on MEOLUT for global coverage then
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a developmental MEOLUT should be used in the evaluation. There is no need to have one of each
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type of developmental LUT (MEO, LEO, and GEO) in order to conduct testing.
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Once Council has approved the [SGL] specifications they will be available for LUT manufacturers.
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3.2
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Proof of Concept Phase
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The Proof of Concept (POC) phase will assess the basic capabilities of the SGBs and establish
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preliminary performance levels that can be expected. The results will identify the necessary
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changes to current LUTs and help to guide the development of [SGL] specifications. Additionally,
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knowledge gained during the POC phase will guide development of the Type Approval Standards
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and Acceptance of Testing Facilities for SGBs.
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3-6
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3.2.1
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Proof of Concept Testing
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Prototype beacons and beacon simulators may be developed for the POC phase. The POC phase
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will confirm the capabilities of the SGBs through and MEOSAR space segment. During the SGB
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POC phase, the MEOSAR ground segment is anticipated to be in the latter D&E stages and
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preliminary stages of Early Operational Capability (EOC).
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The primary ground stations to be used during the POC testing will likely be developmental LUTs
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or developmental LUTs updated in order to successfully capture and process the SGB signal. It is
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anticipated that LUT specifications will be developed during the POC phase. POC testing of the
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SGB will aid in the assessment of necessary LUT changes. Developmental LUTs may eventually
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be commissioned into the operational SGB/LUT system once the commissioning standards are
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approved. Interested Participants will develop an SGB POC test plan and share their test results
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with the Cospas-Sarsat Council.
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POC testing will include at a minimum:
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a) confirmation of the ability to reliably receive and process SGB signals through the space
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segment (i.e., confirmation of the performance of the link from the beacon to the satellite
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and the ground station);
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b) assessment of the detection capability and independent location accuracy that may be
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achieved with the new SGBs in the existing Cospas-Sarsat System;
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c) assessment of necessary changes to existing LUT segment in order to fully process and
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decode SGBs;
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d) assessment of performance of SGBs by [SGL]s that have been upgraded or developmental
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LUTs designed to be fully compatible with SGBs.
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Global availability of SGB capable LUTs is not envisioned during this phase. Cospas-Sarsat
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Participants with ground segment equipment capable of receiving and processing the SGB bursts
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should be invited to participate in the proof-of-concept trials. There will be no distribution of
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operational distress alert data to SAR services during the proof-of-concept phase.
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The POC phase will be completed once the prototype SGBs and developmental [SGL]s have gone
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through described tests and proven an acceptable level of performance.
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3.2.2
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Modifications of other Relevant Cospas-Sarsat Documents
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The development of SGB/[SGL] specifications will likely require changes to other Cospas Sarsat
|
|
documents. The extent of the modifications will depend on the magnitude and nature of the
|
|
changes between the current beacon and LUT specifications and SGB and [SGL] specifications.
|
|
For example, change in beacon frequencies, duration of burst transmission or repetition periods
|
|
would impact frequency channel capacity detailed in document C/S T.012 (Frequency
|
|
Management Plan) and the link budget, frequency requirements and coordination procedures
|
|
described in C/S T.014 (Cospas Sarsat Frequency Requirements and Coordination Procedure).
|
|
|
|
3-7
|
|
|
|
Changes in protocols would also require modifications to document C/S G.005 (Cospas-Sarsat
|
|
Guideline on 406 MHz Beacon Coding, Registration and Type Approval).
|
|
It is anticipated that approval of modifications to the other documents would not be required for
|
|
type approval of second generation beacons, but would be needed prior to the deployment of the
|
|
second generation beacons. Amendments to these documents are expected to be made during the
|
|
POC phase.
|
|
3.2.3
|
|
Development of SGB Type Approval Standards and Acceptance of Test Facilities
|
|
This task will begin during the POC phase. The knowledge gained through POC testing will aid
|
|
the development of the SGB Type Approval Standards (C/S T.021).
|
|
Test facilities that perform Cospas-Sarsat type approval will need to make modifications to testing
|
|
hardware and software. Furthermore, the test facilities will need to demonstrate their ability to
|
|
accurately gauge SGB performance. As such, modification of C/S T.008 (Cospas Sarsat
|
|
Acceptance of 406 MHz Beacon Type Approval Test Facilities) should commence in parallel with
|
|
development of the new Type Approval Standards.
|
|
It is anticipated that the SGB TA standard (C/S T.021) and Acceptance of Beacon Test Facilities
|
|
will be further developed during the SGB/[SGL] Transition phase.
|
|
3.3
|
|
Transition to Operations Phase
|
|
3.3.1
|
|
Documentation Revisions and Finalizations
|
|
This task will involve revisions to the [SGL] specifications and commissioning standards. MCC
|
|
documents will need to be modified, in particular, documents C/S A.001 (Data Distribution Plan),
|
|
A.002 (Standard Interface Description), A.005 (MCC Performance Specification and Design
|
|
Guidelines), and A.006 (MCC Commissioning Standard). Other Cospas-Sarsat documents may
|
|
also need to be updated. Before release of SGB beacons into the market place, all documents that
|
|
are identified as requiring an update must be approved by the Cospas-Sarsat Council.
|
|
3.3.2
|
|
Second Generation LUT Commissioning Standards
|
|
This task will use the knowledge gained during the POC testing of expected [SGL] performance
|
|
to generate a commissioning standard. These commissioning standards will be used to certify that
|
|
a LUT is capable of processing SGB transmissions and distributing appropriate alert data to an
|
|
associated SGB capable MCC (SGM). A commissioned ground
|
|
segment with global coverage will be necessary to allow SGBs to be type approved and used
|
|
operationally.
|
|
|
|
3-8
|
|
|
|
3.3.3
|
|
Second Generation Beacon and Second Generation Ground Segment System
|
|
Testing
|
|
In order to participate in SGB System testing, Participants will need to upgrade existing LUTs or
|
|
procure [SGL]s. Once at least one SGB capable LUT is available, and a System Test Plan has been
|
|
coordinated with other participants, the SGB Systems Test phase can commence. Participants will
|
|
coordinate SGB System testing and share their results with Cospas-Sarsat. SGB System Test
|
|
participants shall consider the impact to the existing LEO/GEO/MEO systems by SGB System
|
|
tests and ensure it is minimized. In case a LUT is involved in SGB System tests and is also used
|
|
operationally (for MEOSAR or GEOSAR operations), priority shall be given to first generation
|
|
beacon processing if possible.
|
|
A demonstration of SGB performance may be required for national and international organizations
|
|
(e.g., ICAO and IMO which mandate the use of beacons and accept distress alerting systems, ITU
|
|
which regulates the use of the frequency bands, and Cospas-Sarsat Participants that provide and
|
|
use the new alerting system) to accept SGBs as an alerting source.
|
|
The transition to SGBs and a ground segment capable of receiving SGB transmissions will have
|
|
to be done while maintaining full global C/S operational capability for first generation beacons.
|
|
All Cospas-Sarsat Participants will be invited to participate in the SGB System Test. Successful
|
|
completion of SGB System Test activities should contribute necessary data to support a Council
|
|
decision on the operational use of SGBs.
|
|
3.3.4
|
|
Test Facilities Prepare for SGB Type Approval Tests
|
|
This activity includes the work to be undertaken by 406 MHz beacon type approval test facilities
|
|
to modify their equipment and test set-up in preparation for type approval testing of second
|
|
generation beacons. Acceptance of test facilities using C/S T.008 would require that test facilities
|
|
successfully demonstrate that their equipment and procedures comply with the new Cospas-Sarsat
|
|
type approval procedure (C/S T.021).
|
|
Test laboratories may initiate this activity while the beacon specification and type approval
|
|
procedures are being developed (in particular for new tests required to address new features such
|
|
as the return link capability), but this activity may not be completed by some test facilities for
|
|
approximately six months after the approval of SGB TA Standards (T.021). This period is needed
|
|
by facilities to upgrade hardware, software, personnel, processes, etc. to enable them to properly
|
|
perform testing as defined by the SGB TA Standards (T.021). After the test facilities have made
|
|
the proper preparations for SGB Type Approval testing, the Cospas-Sarsat Programme will ensure
|
|
that the modifications made by the test facilities allow these facilities to undertake the new type
|
|
approval procedures.
|
|
3.3.5
|
|
Re-acceptance of Type Approval Test Facilities for SGB Type Approval Tests
|
|
After a test facility has made the proper modifications or additions to their testing equipment, tests
|
|
will be required to demonstrate the test facility's ability to perform SGB testing. Successful
|
|
|
|
3-9
|
|
|
|
completion of these tests will allow the Council to recommend the test facility be accepted for
|
|
performing SGB TA testing.
|
|
Completion of this activity, by at least one of the test laboratories, allows formal Cospas Sarsat
|
|
type approval testing to begin. However, if the ground segment cannot yet support SGB and SGB
|
|
ELT(DT) encoded location positioning, then a Type Approval Certificate will be withheld, and
|
|
placed in a "pending" status, until it is deemed appropriate to be issued by the Council.
|
|
It is anticipated that first Cospas-Sarsat type approval of second generation 406 MHz beacon could
|
|
take place one year after the approval of the new TA standard (T.021) and Acceptance of
|
|
TA Facilities (T.008).
|
|
3.4
|
|
SGB Transition Phase
|
|
[Production of SGBs will not be possible until the SGB specification and type approval standards
|
|
have been approved. Furthermore, sale of SGBs cannot be permitted without global coverage from
|
|
a space and ground segment capable of detecting, independently locating and distributing SGB
|
|
alerts. An exception to the limitation of sales of SGB is an ELT(DT) SGB designed to meet ICAO
|
|
GADSS requirements described in section 3.5.]
|
|
[To declare the start of the SGB transition phase the Cospas-Sarsat Council should:
|
|
a) approve specifications and commissioning requirements for LUTs and MCCs that process
|
|
transmissions or associated information for SGBs; and
|
|
b) approve specifications and type approval standards for SGBs; and
|
|
c) declare at least one SGB-capable MEOLUT and associated SGB-capable MCC as
|
|
commissioned; and
|
|
d) approve amended or new Cospas-Sarsat documentation as appropriate.]
|
|
This transition phase shall be completed when:
|
|
- a global space segment will be available,
|
|
- a global network of LUTs capable of processing Second Generation Beacons, associated
|
|
with MCCs capable of processing SGBs, will be commissioned and ready for operations,
|
|
- a network of MCCs will be capable of distributing SGB alerts globally.
|
|
3.5
|
|
MEOSAR Global Coverage - Encoded Locations (To Accommodate SGB
|
|
ELT(DTs))
|
|
Although the global SGB independent location capability may not be achieved at this time,
|
|
ELT(DT)s with GNSS encoded location capabilities are planned to be available to address the
|
|
Global Aeronautical Distress and Safety System (GADSS) requirements.
|
|
|
|
3-10
|
|
|
|
This milestone will be met when there is global detection coverage for detection of SGBs. A
|
|
ground segment capable of detecting, processing and relaying SGB signals will be commissioned
|
|
at this point. Additionally, a space segment capable of providing MEOSAR global detection for
|
|
SGB's will be available.
|
|
This transition phase shall be completed when:
|
|
- a global space segment will be available,
|
|
- a global network of LUTs capable of processing Second Generation Beacons will be
|
|
commissioned and ready for operations for SGB ELT(DT) detection,
|
|
- a network of MCCs will be capable of distributing SGB ELT(DT) alerts globally.
|
|
For information on the plans associated with MEOSAR implementation (e.g., MEOSAR
|
|
IOC/FOC, etc.) please refer to document C/S R.012, "Cospas-Sarsat 406 MHz MEOSAR
|
|
Implementation Plan".
|
|
3.6
|
|
SGB Full Operational Capability (FOC)
|
|
Full Operational Capability is a declaration by C/S that a system based on the use of SGBs is
|
|
considered fully operational. This implies sufficient space and ground segment components have
|
|
been commissioned in accordance with C/S requirements to provide global coverage for SGBs,
|
|
including global SGB alert distribution. At this point, beacons defined in T.018 and type approved
|
|
according to T.021 can be marketed as an SGB, and used operationally. Beacons defined in T.001
|
|
and type approved according to T.007 will continue to be developed and used operationally, unless
|
|
otherwise decided by the Cospas-Sarsat Council.
|
|
3.6.1
|
|
Type Approval of Second Generation Beacons
|
|
This task consists of the formal Cospas-Sarsat type approval of specific models of 406 MHz second
|
|
generation beacons. The activity requires Council approval of all Cospas-Sarsat second generation
|
|
beacon documents (C/S T.018, C/S T.021) and global coverage of commissioned [SGL]s and
|
|
MCCs.
|
|
Completion of this task is a pre-requisite for the availability of second generation beacon on the
|
|
market. Note that national Administrations would still need to authorize the use of these beacons
|
|
in the Cospas-Sarsat System. This may require additional tests to demonstrate compliance with
|
|
national or international standards.
|
|
3.6.2
|
|
Updates to National and International Standards
|
|
The deployment of second generation 406 MHz beacons requires that administrations approve
|
|
updates to their current national and international standards to make reference to the new beacon
|
|
specification. Given the numerous standards impacted by the process, it is unlikely that all
|
|
standards will be modified simultaneously. However partial deployment of second generation
|
|
|
|
3-11
|
|
|
|
beacons could be allowed as Administrations update their standards for specific types of beacons.
|
|
It is expected that the revision of these standards will be initiated shortly after SGB specifications
|
|
have been approved by Cospas-Sarsat Council and could be completed two years after the approval
|
|
of the beacon specification.
|
|
- END OF SECTION 3 -
|
|
- END OF DOCUMENT -
|
|
|
|
Cospas-Sarsat Secretariat
|
|
1250 Rene-Levesque Blvd. West, Suite 4215, Montreal (Quebec) H3B 4W8 Canada
|
|
Telephone: +1 514 500 7777
|
|
Fax: +1 514 500 7996
|
|
Email: mail@cospas-sarsat.int
|
|
Website: http://www.cospas-sarsat.int |