Ryan Malloy 4ed92efd69 refactor: move spec references out of published site
Cospas-Sarsat specification summaries moved to reference/ for internal
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---
title: "R013: Cospas-Sarsat Meteosat Second Generation"
description: "Official Cospas-Sarsat R-series document R013"
sidebar:
badge:
text: "R"
variant: "note"
# Extended Cospas-Sarsat metadata
documentId: "R013"
series: "R"
seriesName: "Reports"
documentType: "report"
isLatest: true
issue: 1
revision: 1
documentDate: "October 2006"
originalTitle: "Cospas-Sarsat"
---
> **📋 Document Information**
>
> **Series:** R-Series (Reports)
> **Version:** Issue 1 - Revision 1
> **Date:** October 2006
> **Source:** [Cospas-Sarsat Official Documents](https://www.cospas-sarsat.int/en/documents-pro/system-documents)
---
COSPAS-SARSAT
METEOSAT SECOND GENERATION (MSG)
GEOSAR PERFORMANCE
EVALUATION REPORT
C/S R.013
Issue 1 - Revision 1
R13OCT06
MSG PERFORMANCE EVALUATION REPORT
History
Issue
Revision Date
Comments
Approved by CSC-33
Approved by CSC-37
R13OCT06
LIST OF PAGES
Page \#
Date of
Page \#
Date of
latest
latest
revision
revision
cover
Oct 06
E-1
Oct 04
Oct 06
E-2
Oct 04
Oct 06
E-3
Oct 04
Oct 06
E-4
Oct 04
Oct 06
F-1
Oct 04
1-1
Oct 04
F-2
Oct 04
1-2
Oct 04
2-1
Oct 04
2-2
Oct 04
3-1
Oct 04
3-2
Oct 04
3-3
Oct 04
3-4
Oct 04
3-5
Oct 04
3-6
Oct 04
3-7
Oct 04
3-8
Oct 06
3-9
Oct 06
3-10
Oct 06
3-11
Oct 06
3-12
Oct 06
4-1
Oct 04
4-2
Oct 04
A-1
Oct 04
A-2
Oct 04
B-1
Oct 04
B-2
Oct 04
C-1
Oct 04
C-2
Oct 04
D-1
Oct 04
D-2
Oct 04
D-3
Oct 04
D-4
Oct 04
R13OCT06
TABLE OF CONTENTS
Page
1.
INTRODUCTION ..................................................................................................... 1-1
1.1
Background ................................................................................................................. 1-1
1.2
MSG GEOSAR Performance Evaluation ................................................................... 1-1
2.
MSG GEOSAR PERFORMANCE EVALUATION
GOALS AND OBJECTIVES ................................................................................... 2-1
2.1
Performance Evaluation Goals .................................................................................... 2-1
2.2
Objectives .................................................................................................................... 2-1
3.
MSG PERFORMANCE EVALUATION RESULTS ............................................ 3-1
3.1
T-1:
Processing Threshold, System Margin and Beacon Message
Processing Performance ................................................................................ 3-1
3.2
T-2:
Time to Produce Valid, Complete and Confirmed Messages ....................... 3-3
3.3
T-3:
Carrier Frequency Measurement Accuracy .................................................. 3-4
3.4
T-4:
MSG GEOLUT Channel Capacity ............................................................... 3-5
3.5
T-8:
Processing Anomaly Performance ................................................................ 3-6
3.6
T-9:
MSG Coverage.............................................................................................. 3-8
3.7
Complementarity and Effectiveness of the GEOSAR/LEOSAR Systems ............... 3-11
4.
CONCLUSIONS ....................................................................................................... 4-1
R13OCT06
LIST OF ANNEXES
Annex A :
Processing Threshold and System Margin Test Results .......................... A-1
Annex B :
Valid Message Processing Performance ...................................................B-1
Annex C :
Complete and Confirmed Complete Message Performance
Test Results ...............................................................................................C-1
Annex D :
Time to Produce Valid, Complete and Confirmed Complete
Messages Test Results ............................................................................. D-1
Annex E :
Frequency Measurement Accuracy Test Results ...................................... E-1
Annex F :
Capacity Test Results ............................................................................... F-1
LIST OF FIGURES
Figure 3.1 :
Location of MSG Alerts ........................................................................... 3-8
Figure 3.2 :
MSG Footprint Boundary ......................................................................... 3-9
Figure 3.3 :
Eastern Footprint Boundary .................................................................... 3-10
Figure 3.4 :
Northern Footprint Boundary ................................................................. 3-10
LIST OF TABLES
Table 3.1 :
Processing Threshold and System Margin ............................................... 3-2
Table 3.2 :
Valid Message Processing Performance ................................................... 3-3
Table 3.3 :
Complete and Confirmed Complete Message Performance
at Processing Threshold (31 dBm Uplink) ............................................... 3-3
Table 3.4 :
Time to Produce Messages at Processing Threshold (31 dBm Uplink) ... 3-4
Table 3.5 :
Time to Produce Messages at Processing Threshold for the
95th Percentile (31 dBm Uplink) ............................................................... 3-4
Table 3.6 :
Capacity Performance Results Measured by French GEOLUT ............... 3-6
Table 3.7 :
Capacity Performance Results Measured by Spanish GEOLUT ............. 3-6
Table 3.8 :
Processing Anomaly Performance as Function of
Received Beacon Bursts (Measured by Maspalomas GEOLUT)............. 3-7
Table 3.9 :
Processing Anomaly Performance as Function of Number of Alert
Messages Sent to MCC (Measured by Toulouse GEOLUT) ................... 3-8
Table 3.10 :
Complementarity and Effectiveness of
MSG GEOSAR/LEOSAR Systems ........................................................ 3-11
R13OCT04
1 - 1
1.
INTRODUCTION
The European Organisation for the Exploitation of Meteorological Satellites (EUMETSAT)
provides 406 MHz Search and Rescue (SAR) repeaters on their Meteosat Second Generation
(MSG) meteorological satellites. The first of the MSG satellites was launched in
August 2002 and following payload testing the SAR instrument was made available for use
by Cospas-Sarsat Ground Segment operators from October 2002. However, because MSG
satellites were under development when the original Cospas-Sarsat GEOSAR demonstration
and evaluation programme was conducted, its performance had not been tested operationally.
In view of this the Cospas-Sarsat Council directed that prior to formal inclusion as part of the
operational Cospas-Sarsat System, a MSG GEOSAR performance evaluation programme
should be conducted to:
a.
measure MSG GEOSAR / GEOLUT performance; and
b.
establish specification and commissioning requirements for GEOLUTs which operate
with the MSG GEOSAR payload.
1.1
Background
From 1996 to 1998 Cospas-Sarsat conducted a demonstration and evaluation programme to
determine the suitability of using satellites in geostationary orbit equipped with SAR
instruments to process the signals from Cospas-Sarsat 406 MHz distress beacons. This
programme, hereafter referred to as the GEOSAR D & E, was implemented using the GOES
series of satellites provided by the USA, the Insat-2 satellites provided by India, and
experimental ground segment equipment provided by Canada, Chile, India, Spain and the
United Kingdom. The GEOSAR D & E demonstrated that GEOSAR satellites provided a
significant enhancement to the Cospas-Sarsat system. Following from this conclusion, in
October 1998 the Cospas-Sarsat Council decided that the 406 MHz GEOSAR system
components should be incorporated into the Cospas-Sarsat System as soon as possible. A
summary report of the Cospas-Sarsat GEOSAR D&E is available from the Cospas-Sarsat
web site as document C/S R.009. The complete report is also available from the Cospas-
Sarsat Secretariat on request.
1.2
MSG GEOSAR Performance Evaluation
During the period that the GEOSAR D & E was being conducted, EUMETSAT was
developing a 406 MHz repeater for their MSG satellites that would be capable of relaying the
signals from Cospas-Sarsat 406 MHz distress beacons.
Because the technical characteristics of the MSG SAR instrument are different from SAR
instruments on the GOES and the Insat-2 satellites, the tests reported herein were conducted
to establish MSG GEOSAR / GEOLUT performance, and any specific GEOLUT
specification and commissioning requirements.
R13OCT04
1 - 2
The administrations of France, Spain and the United Kingdom provided and operated the
GEOLUTs that participated in the MSG performance evaluation.
The tests reported herein were performed while the MSG-1 satellite was at its final operating
position of 3.4 W. France's 406 MHz beacon simulator with a linearly polarised whip
antenna was used to transmit the uplink signals developed specifically for the testing.
- END OF SECTION 1 -
R13OCT04
2 - 1
2.
MSG
GEOSAR
PERFORMANCE
EVALUATION
GOALS
AND
OBJECTIVES
2.1
Performance Evaluation Goals
The goals of the performance evaluation programme were to:
a.
characterize the technical performance of the MSG GEOSAR / GEOLUT system and
confirm whether MSG GEOSAR satellite / GEOLUT systems would be effective for
providing useful 406 MHz alert data; and
b.
validate specification and commissioning requirements for GEOLUTs which would
operate with the MSG satellite.
2.2
Objectives
The programme was subdivided into specific technical objectives. Each objective was
addressed by conducting tests and analysing the results. The tests were similar to the
technical tests conducted in the previous GEOSAR D&E. Where necessary the procedures
were modified to gain additional information that would be necessary to develop MSG
GEOLUT specification and commissioning requirements. Most of the tests required a
beacon simulator whose power output and message could be accurately controlled.
An overview of each objective is listed below:
T-1
Processing Threshold, System Margin, and Beacon Message Processing Performance
Determine the processing threshold, processing performance, system margin and the
performance in respect of long format beacon messages for GEOLUTs which operate
with the MSG payload. The beacon test signals used to assess these parameters do
not include beacon messages that collide with each other.
T-2
Time to Produce Valid and Confirmed Messages
Determine the statistical distribution of the time required for the GEOLUT to produce
valid and confirmed beacon messages. The beacon test signals used to assess this
parameter do not include beacon messages which collide with each other.
T-3
Carrier Frequency Measurement Accuracy
Determine how accurately the beacon carrier frequency can be determined by the
MSG GEOSAR / GEOLUT system. The beacon test signals used to assess this
parameter do not include beacon messages which collide with each other.
T-4
MSG GEOLUT Channel Capacity
Assess the capability of the GEOSAR system to handle multiple simultaneously
active distress beacons in a single 406 MHz channel. This parameter is assessed by
generating traffic loads which include beacon messages which collide with each other.
R13OCT04
2 - 2
T-5
Impact of Interference
Monitor the band for the presence of interference while the tests are being performed,
in order to understand any anomalies in the results and to illustrate the ability of the
GEOSAR system to provide valid messages in the presence of interference and noise
in the frequency bands used by the MSG GEOSAR system.
T-6
Impact of Interference From LEOSAR Satellites
Assess the impact of interference from LEOSAR satellite downlink signals on the
ability of the GEOLUT to produce valid and confirmed alert messages.
T-7
MSG GEOLUT Network Performance
Determine if at a given time some GEOLUTs are affected by interference from the
LEOSAR system, the expected GEOSAR alerts would continue to be reliably
provided by other GEOLUTs in the MSG ground segment.
T-8
Processing Anomalies
Assess the performance of the GEOLUT in respect of the production of processing
anomalies.
T-9
MSG Coverage
Estimate the geographic coverage of the MSG GEOSAR system.
- END OF SECTION 2 -
R13OCT06
3 - 1
3.
MSG PERFORMANCE EVALUATION RESULTS
3.1
T-1: Processing Threshold, System Margin, and Beacon Message Processing
Performance
The processing threshold, processing performance and the system margin are "figures of
merit" of the GEOLUT, as defined below.
Processing Threshold
The processing threshold is the value of the minimum carrier to noise density ratio (C/N0) at
the GEOLUT processor for which the GEOLUT is able to produce a valid message for a
beacon event 99% of the time (the lower this value the more sensitive the GEOLUT). Equally
the processing threshold can be expressed in terms of the minimum beacon effective isotropic
radiated power (EIRP) for which the GEOLUT is able to produce a valid message 99% of the
time.
System Margin
The system margin is the difference between a nominal beacon (which by definition is a
beacon with an EIRP of 37 dBm) and a beacon operating at the GEOLUT threshold.
Valid Message Processing Performance
Valid message processing performance is the minimum EIRP for which the MSG GEOLUT
can produce a valid message for the beacon event within 5 minutes of beacon activation 95%
of the time. The valid message processing performance can also be expressed in terms of the
C/N0 at the GEOLUT that produces this level of performance.
Long Message Processing Performance
At present Cospas-Sarsat does not have a GEOLUT specification requirement for producing
complete and confirmed long messages. Nevertheless, with the increased use of location
protocol beacons using the long message format, it is necessary to assess the MSG system
performance in this regard.
3.1.1
Methodology and Data Collection
A beacon simulator with a linearly polarised whip antenna was used to replicate distress
beacons that transmit long format messages at specific EIRPs. 20 bursts were transmitted for
each beacon identification which simulated a beacon being active for approximately 17
minutes. Hereafter the term "beacon event" is used to describe a beacon being active for a
period of time. Schedule constraints and equipment availability required the test to be
conducted in three parts, two parts comprising 25 beacon events each and the other
comprising 50 beacon events. In total 100 beacon events for each EIRP were transmitted,
whilst ensuring that signals from individual beacon events did not overlap in time and
frequency with the signals from other beacon events. The uplink EIRP of the test signals
were calibrated to within +/- 1 dB. The output of the GEOLUT was monitored and the time
required to produce valid, complete and complete confirmed messages for each beacon event
R13OCT06
3 - 2
was captured. The procedure was repeated at EIRP values ranging from 38 dBm to 29 dBm,
in one dB increments.
The UK and Spanish GEOLUTs were still under development during some of the testing, and
were not available to participate in all 100 beacon events that were transmitted.
Consequently the UK and Spanish performance was evaluated based on a reduced sample set
of 75 and 50 beacon events respectively.
3.1.2
Processing Threshold and System Margin
The processing threshold and system margin as evaluated by the French, Spanish and UK
GEOLUTs are provided at Table 3.1 below. The detailed results are provided at Annex A.
Table 3.1: Processing Threshold and System Margin
GEOLUT
THRESHOLD
EIRP
(dBm)
THRESHOLD
GEOLUT C/N0
(dB-Hz)
SYSTEM
MARGIN
(dB)
NUMBER OF
BEACON
EVENTS USED
France
26.4\*
Spain
30.9
UK
26.9\*
\*
During the test period, the French and UK GEOLUTs had an error with their C/N0
calculations that caused them to systematically report C/N0 4 dB too low. When this
anomaly is taken into account all three GEOLUTs had very similar processing
performance.
The results indicated that beacon signals greater than 31 dBm will be reliably detected by the
MSG GEOSAR system. Below the threshold of 31 dBm the system performance degrades
rapidly, with only a small percentage of the signals being detected with uplink EIRP values
less than 30 dBm.
3.1.3 Valid Message Processing Performance
The valid message processing performance is a measure of the GEOSAR system's ability to
provide a valid message within 5 minutes of beacon activation 95% of the time.
The minimum uplink EIRP required for the GEOLUTs to provide valid messages within 5
minutes is provided at Table 3.2 below. The detailed results are provided at Annex B.
R13OCT06
3 - 3
Table 3.2: Valid Message Processing Performance
GEOLUT
THRESHOLD
EIRP
(dBm)
THRESHOLD
GEOLUT C/N0
(dB-Hz)
NUMBER OF
BEACON
EVENTS USED
France
27.0
Spain
30.9
UK
26.9
The 3 GEOLUTs satisfied the message processing requirement for uplink signals with an
EIRP of 31 dBm. The results for the Toulouse GEOLUT dropped slightly below the 95th
percentile (i.e. 93%) for the test signals at 32 dBm. However, subsequent tests confirmed the
GEOLUT message processing performance at this level. This seems to indicate that the
anomaly, which was experienced to a lesser degree by the Maspalomas GEOLUT, was
probably caused by interference during the test.
3.1.4 Complete and Confirmed Complete Message Performance
The performance of the French, Spanish and UK GEOLUTs to produce complete and
confirmed complete messages for beacons with uplink signals at the system threshold level of
30 dBm is provided at Table 3.3 below. The detailed performance of each GEOLUT at all
measured uplink signals is provided at Annex C.
Table 3.3:
Complete and Confirmed Complete Message Performance at Processing
Threshold (31 dBm Uplink)
GEOLUT
COMPLETE
MESSAGE
PROBABILITY
CONFIRMED
COMPLETE
MESSAGE
PROBABILITY
NUMBER OF
BEACON
EVENTS USED
France
0.99
0.96
Spain
1.00
1.00
UK
1.00
0.97
3.2
T-2: Time to Produce Valid, Complete and Confirmed Messages
This test assesses how long it takes GEOLUTs operating with the MSG satellite to produce
valid beacon messages, complete long messages, and confirmed complete long messages.
3.2.1
Methodology and Data Collection
For simplicity this test was conducted by analysing the data collected for test T-1
(Threshold). Note that the T-1 test scenario is specifically designed not to generate beacon
bursts which overlap in time and frequency. Consequently, for operational beacon events, the
times to produce valid, complete, and the time to confirm complete messages may differ from
those determined during this test.
R13OCT06
3 - 4
3.2.2 Time to Produce Valid, Complete and Confirmed Complete Messages at
Threshold
Table 3.4 provides statistics in respect of the average time required for the French, Spanish
and UK GEOLUTs to produce valid, complete and confirmed complete messages for beacon
signals at threshold.
Table 3.4:
Time to Produce Messages at Processing Threshold (31 dBm Uplink)
GEOLUT
VALID MESSAGES
Avg / Standard Deviation
(Seconds)
COMPLETE MESSAGES
Avg / Standard Deviation
(Seconds)
CONFIRMED COMPLETE
MESSAGES
Avg / Standard Deviation
(Seconds)
France
67 / 106\*
166 / 189\*
376 / 217\*
Spain
36 / 55
97 / 143
223 / 198
UK
29.3 / 50.7
70.3 / 184.5
300.7 / 204.9
* Statistics calculated from 50 beacon events (not 100 as reported at tables 3.1, 3.2 and 3.3)
Table 3.5 provides statistics in respect of the time required to produce valid, complete and
confirmed complete messages for the 95th percentile, in respect of beacon signals that
transmit at the processing threshold of 30 dBm.
Table 3.5:
Time to Produce Messages at Processing Threshold for the 95th Percentile
(31 dBm Uplink)
GEOLUT
VALID MESSAGES
(Seconds)
COMPLETE MESSAGES
(Seconds)
CONFIRMED COMPLETE
MESSAGES
(Seconds)
France
252\*
552\*
852\*
Spain
UK
* Statistics calculated from 50 beacon events (not 100 as reported at tables 3.1, 3.2 and 3.3)
The detailed data providing the time required for the GEOLUTs to produce valid, complete
and confirmed complete messages for signals with different transmit EIRPs are provided at
Annex D.
3.3
T-3: Carrier Frequency Measurement Accuracy
This test assessed how accurately MSG GEOSAR / GEOLUTs could measure the beacon
transmit frequency. For each valid message produced by the GEOLUT the frequency
measured was compared against the known transmit frequency provided by the beacon
simulator operator.
3.3.1
Methodology and Data Collection
For simplicity, this test was conducted by analysing the data collected for test T-1. For each
beacon event the frequency measurement provided by the GEOLUT for the first valid
message produced was recorded.
R13OCT06
3 - 5
The GEOLUT measured frequency included any calibration that would normally be
performed during actual GEOLUT operations (e.g. if the GEOLUT includes features for
assessing and correcting frequency measurements by applying calibration correction factors
and using reference beacons, these features should be activated).
3.3.2 Frequency Measurement Accuracy Results
The detailed results for the frequency measurement accuracy testing is provided at Annex E.
In summary the French, Spanish and UK GEOLUTs reliably measured the frequency to
within the Cospas-Sarsat GEOLUT specification of 2 Hz for all signals at or above the
processing threshold. However, given the impact that periods of solar eclipse has on the
satellite frequency stability, this level of performance might not be experienced at all times.
All the GEOLUTs needed at least two reference beacons in the MSG satellite footprint for
frequency measurement calibration to accommodate frequency variations during the eclipse
period. At other times the Toulouse reference beacon alone was sufficient for frequency
calibration. Since both the Toulouse time calibration beacon and the UK reference beacon
are within the MSG satellite footprint, no additional reference beacons are required for this
function.
3.4
T-4: MSG GEOLUT Channel Capacity
The definition of capacity in Cospas-Sarsat GEOSAR systems is the number of 406 MHz
distress beacons operating simultaneously in the field of view of a GEOSAR satellite that can
be successfully processed by the System to provide a valid beacon message, under nominal
conditions, within 5 minutes of beacon activation 95% of the time.
3.4.1
Methodology and Data Collection
The MSG GEOSAR channel capacity was assessed by generating traffic loads equivalent to
known numbers of simultaneously active long format beacons in a Cospas-Sarsat 406 MHz
channel. The time required for the GEOLUT to produce a valid beacon message, complete
message and confirm a complete message for each beacon event was recorded. The number
of simultaneously active beacon events was changed and the time required for the GEOLUT
to produce valid, complete and complete confirmed messages was calculated and recorded
for the new 406 MHz traffic load.
The test scripts transmitted by the beacon simulator conformed to the nominal conditions
detailed in the Cospas-Sarsat 406 MHz frequency management plan (document C/S T.012),
with the exception that the uplink EIRP was selected to be 35 dBm rather than 32 dBm. The
test replicated a number of beacon messages overlapping in time and frequency
commensurate with the number of simultaneously active beacons. Further, the beacon events
used in the test script also replicated the beacon burst repetition period defined in document
C/S T.001 (406 MHz beacon specification). The test was scheduled to avoid any potential
interference caused by Cospas-Sarsat LEOSAR satellite downlink transmissions.
R13OCT06
3 - 6
To obtain a sufficient sample size 10 different test scripts were transmitted for each simulated
beacon traffic load. For example 10 scripts simulating 15 simultaneously active beacons
were transmitted, which resulted in a sample size of 150 active beacons for this traffic load.
3.4.2 Capacity Results
This test was performed by the French and the Spanish GEOLUTs, and the resulting
performance statistics are provided at Tables 3.6 and 3.7 respectively.
Table 3.6:
Capacity Performance Results Measured by French GEOLUT
NUMBER OF
ACTIVE
BEACONS
PROBABILITY
OF VALID
MESSAGE
WITHIN 5 MIN
PROBABILITY
OF VALID
MESSAGE
WITHIN 10 MIN
PROBABILITY
OF VALID
MESSAGE
WITHIN 15 MIN
PROBABILITY
OF CONFIRMED
COMPLETE
MESSAGE
WITHIN 15 MIN
0.98
0.99
1.00
0.99
0.97
1.00
1.00
0.98
0.87
0.98
1.00
0.94
0.93
1.00
1.00
0.98
Table 3.7:
Capacity Performance Results Measured by Spanish GEOLUT
NUMBER OF
ACTIVE
BEACONS
PROBABILITY
OF VALID
MESSAGE
WITHIN 5 MIN
PROBABILITY
OF VALID
MESSAGE
WITHIN 10 MIN
PROBABILITY
OF VALID
MESSAGE
WITHIN 15 MIN
PROBABILITY
OF CONFIRMED
COMPLETE
MESSAGE
WITHIN 15 MIN
1.00
1.00
1.00
1.00
0.99
1.00
1.00
1.00
0.99
1.00
1.00
0.95
0.99
1.00
1.00
0.99
The results indicate that for beacon populations with uplink EIRP values exceeding 35 dBm,
the capacity would exceed 20 simultaneously active beacons, and that at this load the MSG
GEOSAR system would reliably provide complete confirmed beacon messages.
3.5
T-8: Processing Anomaly Performance
A processing anomaly is an alert generated by the system that does not correspond to a real
beacon. Processing anomalies may occur when bit errors cause a real beacon transmission to
be received garbled in a manner such that the corrupted message passes BCH error checking.
The beacon message content validation checks at the MCC are able to identify most
processing anomalies, thereby preventing their further distribution as false alerts.
Two different tests were conducted to evaluate the processing anomaly characteristics of the
MSG system. One test measured the processing anomaly rate as a function of the number of
beacon bursts seen by the satellite, and the other test evaluated a processing anomaly rate as a
ratio of the number of processing anomalies sent to the MCC in comparison to the total
number of alerts transmitted by the GEOLUT.
R13OCT06
3 - 7
3.5.1
Processing Anomaly as a Function of Number of Beacon Bursts
This test was conducted by monitoring the 406 MHz channel (406.022 MHz) used by
Cospas-Sarsat reference beacons, and noting instances where the GEOLUT produced valid
beacon messages which did not correspond to any of the reference beacons in the coverage
area of the MSG satellite. Since the identification (IDs) of all reference beacons in view of
the MSG satellite are known, it was inferred that beacons detected in the 406.022 MHz
channel that did not correspond to known reference beacons were processing anomalies.
The time of each processing anomaly was noted and correlated against LEOSAR passes over
the GEOLUT to determine whether interference from LEOSAR satellite downlinks
influenced the processing anomaly performance. The testing took place over 30 days and the
results are summarised in the table below.
Table 3.8:
Processing Anomaly Performance as Function of Received Beacon Bursts
(Measured by Maspalomas GEOLUT)
Number of Bursts
Number of
Processing
Anomalies
Processing
Anomaly Rate
All Data
224,640
0.030%
GEOLUT in LEOSAR Footprint
56,160
0.030%
The results provided by the Spanish GEOLUT indicate that that 3 processing anomalies were
produced for every 10,000 beacon bursts, and that possible interference from LEOSAR
satellite downlinks did not appear to affect performance in respect of processing anomalies.
3.5.2
Processing Anomaly as Percentage of Alerts Transmitted by GEOLUT
This test was conducted by monitoring the alert messages sent by the Toulouse GEOLUT to
the French MCC, and noting those alerts that failed message validation checks at the MCC.
It was assumed that:
a.
the alerts failing beacon message validation were processing anomalies; and
R13OCT06
3 - 8
b.
given the robust validation checks at the MCC for most beacon message protocols,
very few processing anomalies were not detected by the MCC checks. The data was
collected over a two month period from 27 March 2004 to 27 May 2004. For
comparison purposes processing anomaly data was also collected from the two
Toulouse LEOLUTs.
Table 3.9:
Processing Anomaly Performance as Function of Number of Alert
Messages Sent to MCC
(Measured by Toulouse GEOLUT)
Alerts
Transmitted to
MCC
Processing
Anomalies
Transmitted to
MCC
Processing
Anomaly Rate
Toulouse MSG GEOLUT 2273
6,904
3.04%
LEOLUT 2271
7,352
1.28%
LEOLUT 2272
7,605
1.33%
3.6
T-9: MSG Coverage
Two methods were used to evaluate the coverage of the MSG satellite. One method involved
plotting the location of alerts received by the MSG system. The location information was
provided in most cases by the LEOSAR system. The second method involved placing
beacons on ships that were travelling through the MSG coverage boundaries.
The location of alerts that were detected by the MSG system over a 101 day period is
provided at Figure 3.1 below. The footprint circle indicated on Figure 3.1 represents a 0°
elevation from the earth to the satellite.
Figure 3.1:
Location of MSG Alerts
MSG-1 GEOSAR Coverage
27 Jan. - 7 May 2004
R13OCT06
3 - 9
The location of the alerts in Figure 3.1 indicates that the System detects alerts throughout its
coverage area.
The results of a test with a beacon mounted on a ship travelling around the world are
provided at Figure 3.2. The findings demonstrate reception throughout the MSG satellite
footprint for elevation angles greater than 7.7, except for a gap between 37 and 52 East.
Investigation into this gap revealed the presence of a strong interfering signal, which
disrupted reception. As indicated at Figure 3.3 the MSG was able to detect the beacon down
to the horizon, although reliable coverage at the Eastern boundary was achieved for elevation
angles greater than 7.7.
Figure 3.2:
MSG Footprint Boundary
MSG-1 GEO COVERAGE - GEOLUT 2273 TOULOUSE
-180 -165 -150 -135 -120 -105
R13OCT06
3 - 10
Figure 3.3:
Eastern Footprint Boundary
The receptions received from a beacon mounted on a vessel operating at the northern limits
of the MSG coverage are depicted below at Figure 3.4. The results confirmed that the MSG
system could reliably detect transmission at latitudes of 79.229N.
Figure 3.4:
Northern Footprint Boundary
79.229 N
R13OCT06
3 - 11
3.7
Complementarity and Effectiveness of the GEOSAR/LEOSAR Systems
The complementarity and effectiveness of GEOSAR/LEOSAR systems is an assessment of
the percentage of 406 MHz beacon transmissions, within the coverage area of a particular
geostationary satellite, that are detected by only the GEOSAR system, only the LEOSAR
System, or by both systems. This analysis measures the ability of the GEOSAR system to
detect beacons within the satellite coverage area using confirmed detections by the LEOSAR
System as a reference. GEOSAR data for this analysis was provided from the Toulouse MSG
GEOLUT.
Table 3.10: Complementarity and Effectiveness of MSG GEOSAR/LEOSAR Systems
Feb.
%
April
%
Total number of C/S 406 MHz Beacon Activations (BA)
within the FMCC Service Area of the MSG-1 footprint
(Position confirmed by LEO satellite passes, or by RCC
feedback):
Number of BA that were detected using the MSG-1 SAR
signal:
76 %
73 %
Number of BA for which the MSG-1 detection was the
only means of alert:
10 %
13 %
Number of BA for which the MSG-1 detection was the
first means of alert:
54 %
41 %
Number of BA for which the MSG-1 detection was the
first OR only Alert:
64 %
54 %
Number of BA not detected by the MSG-1 GEOLUT 2273:
24 %
26 %
- END OF SECTION 3 -
R13OCT06
3 - 12
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R13OCT04
4 - 1
4.
CONCLUSIONS
The MSG GEOSAR performance evaluation test results show that the MSG GEOSAR
system reliably detects beacons with uplink EIRPs greater than 30 dBm. Furthermore at the
31 dBm threshold the system also reliably provides confirmed complete beacon messages.
The ability to provide confirmed complete messages indicates that the MSG GEOSAR
system will effectively provide MCCs with precise encoded location information when this
data is transmitted in location protocol beacons.
The results achieved by the French, Spanish and United Kingdom GEOLUTs were consistent
with each other. Prior to conducting the testing the design and configuration of the MSG
GEOLUTs had been optimised for overall system performance. Consequently, further major
improvements to GEOLUT performance should not be expected, and the results obtained
during the system evaluation were suitable for developing MSG GEOLUT specification and
commissioning requirements.
- END OF SECTION 4 -
R13OCT04
4 - 2
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R13OCT04
________________________________________________________
ANNEXES TO THE
COSPAS-SARSAT
METEOSAT SECOND GENERATION (MSG)
GEOSAR PERFORMANCE
EVALUATION REPORT
_________________________________________________________
R13OCT04
page left blank
R13OCT04
A - 1
ANNEX A
PROCESSING THRESHOLD AND SYSTEM MARGIN TEST RESULTS
1.0
Processing Threshold and System Margin Test Results Measured by France's GEOLUT
0.90
0.91
0.92
0.93
0.94
0.95
0.96
0.97
0.98
0.99
1.00
Probability of Valid Message
EIRP (dBm)
Processing
Threshold
= 30 dBm
37 dBm
System Margin = 7 dB .
2.0
Processing Threshold and System Margin Test Results Measured by Spain's GEOLUT
Processing Threshold
29.5
30.5
31.5
32.5
33.5
34.5
35.5
36.5
37.5
0.00%
10.00%
20.00%
30.00%
40.00%
50.00%
60.00%
70.00%
80.00%
90.00%
100.00%
Probability of Valid Message
EIRP (dBm)
Systen
Margin
6 dB
.
System
Margin
6 dB
R13OCT04
A - 2
3.0
Processing Threshold and System Margin Test Results Measured by UK's GEOLUT
Processing Threshold
0.0%
10.0%
20.0%
30.0%
40.0%
50.0%
60.0%
70.0%
80.0%
90.0%
100.0%
Probability of Valid Message
EIRP (dBm)
- END OF ANNEX A -
7 dB System
Margin
R13OCT04
B - 1
ANNEX B
VALID MESSAGE PROCESSING PERFORMANCE
1.0
Valid Message Processing Performance Test Results Measured by France's GEOLUT
0.90
0.91
0.92
0.93
0.94
0.95
0.96
0.97
0.98
0.99
1.00
Probability of Valid Message within 5 minutes
EIRP (dBm)
Processing
Performance
= 31 dBm
2.0
Valid Message Processing Performance Test Results Measured by Spain's GEOLUT
Valid Message Processing Performance
29.5
30.5
31.5
32.5
33.5
34.5
35.5
36.5
37.5
0%
10%
20%
30%
40%
50%
60%
70%
80%
90%
100%
Probability of Valid message within 5 minutes
EIRP (dBm)
PROCESSING
PERFORMANCE
R13OCT04
B - 2
3.0
Valid Message Processing Performance Test Results Measured by UK GEOLUT
Valid Message Processing Performance
0.0%
10.0%
20.0%
30.0%
40.0%
50.0%
60.0%
70.0%
80.0%
90.0%
100.0%
Probability of Valid Message Within 5 Minutes
EIRP (dBm)
- END OF ANNEX B -
R13OCT04
C - 1
ANNEX C
COMPLETE AND CONFIRMED COMPLETE MESSAGE
PERFORMANCE TEST RESULTS
1.0
Complete and Confirmed Complete Performance Test Results Measured by France's
GEOLUT
0.90
0.91
0.92
0.93
0.94
0.95
0.96
0.97
0.98
0.99
1.00
Probability of Successful Message Processing
EIRP (dBm)
Confirmed Complete
Complete
2.0
Complete and Confirmed Complete Performance Test Results Measured by Spain's
GEOLUT
Long Message Processing Performance
29.5
30.5
31.5
32.5
33.5
34.5
35.5
36.5
37.5
0.00%
10.00%
20.00%
30.00%
40.00%
50.00%
60.00%
70.00%
80.00%
90.00%
100.00%
Probability of Complete Message
EIRP (dBm)
Probability of Complete Message
Probability of Confirmed Complete Message
R13OCT04
C - 2
3.0
Confirmed Complete Performance Test Results Measured by UK's GEOLUT
Message Performance Test Results
0%
10%
20%
30%
40%
50%
60%
70%
80%
90%
100%
EIRP (dBm)
Probability of Successful Message Processing
- END OF ANNEX C -
Complete Messages
Confirmed Complete Messages
R13OCT04
D - 1
ANNEX D
TIME TO PRODUCE VALID, COMPLETE AND CONFIRMED COMPLETE
MESSAGES TEST RESULTS
1.0
Time to Produce Valid, Complete and Confirmed Complete Message Test Results
Measured by France's GEOLUT
Average Time to Produce Valid, Complete and
Confirmed Complete Messages
Seconds
EIRP (dBm)
Confirmed Complete
Complete
Valid
30/04/04
27/04/04 and
30/04/04 and
25/05/04
2.0
Time to Produce Valid, Complete and Confirmed Complete Message Test Results
Measured by Spain's GEOLUT
29.5
30.5
31.5
32.5
33.5
34.5
35.5
36.5
37.5
Time (s)
EIRP (dBm)
ATVM (sec)
ATCM (sec)
ATCCM (sec)
R13OCT04
D - 2
95th Percentile
29.5
30.5
31.5
32.5
33.5
34.5
35.5
36.5
37.5
Time (s)
EIRP (dBm)
Valid
Complete
Complete Confirmed
98th Percentile
29.5
30.5
31.5
32.5
33.5
34.5
35.5
36.5
37.5
Time (s)
EIRP (dBm)
Valid
Complete
Complete Confirmed
R13OCT04
D - 3
3.0
Time to Produce Valid, Complete and Confirmed Complete Message Test Results
Measured by UK's GEOLUT
Average Time to Message
0.0
100.0
200.0
300.0
400.0
500.0
600.0
700.0
800.0
900.0
1000.0
EIRP (dBm)
Average Time (Seconds)
95th Percentile Time to Messages
-100.0
0.0
100.0
200.0
300.0
400.0
500.0
600.0
700.0
800.0
900.0
1000.0
EIRP (dBm)
95th Percentile Time (Seconds)
Avg Time to Produce Valid Messages
Avg Time to Produce Complete Messages
Avg Time to Produce Confirmed Complete Messages
Avg Time to Produce Valid Messages
Avg Time to Produce Complete Messages
Avg Time to Produce Confirmed
Complete Messages
R13OCT04
D - 4
98th Percentile Time to Messages
-100.0
0.0
100.0
200.0
300.0
400.0
500.0
600.0
700.0
800.0
900.0
1000.0
EIRP (dBm)
98th Percentile Time (Seconds)
- END OF ANNEX D -
Avg Time to Produce Valid Messages
Avg Time to Produce Complete Messages
Avg Time to Produce
Confirmed Complete
Messages
R13OCT04
E - 1
ANNEX E
FREQUENCY MEASUREMENT ACCURACY TEST RESULTS
1.0
Frequency Measurement Accuracy Test Results Measured by France's GEOLUT
Test T3. Carrier Frequency Measurement
30.0
30.5
31.0
31.5
32.0
EIRP (dBm)
Average (Hz)
29/03/04
Test T3. Carrier Frequency Measurement
0.0
0.5
1.0
1.5
2.0
EIRP (dBm)
Standard Deviation Freq.
Measurement Error (Hz)
29/03/04
R13OCT04
E - 2
2.0
Frequency Measurement Accuracy Test Results Measured by Spain's GEOLUT
Carrier Frequency Measurement Acuraccy
27.8
28.8
29.8
30.8
31.8
32.8
33.8
EIRP (dBm)
Avg Freq Measurement Difference (Hz)
Carrier Frequency Measurement Standard Deviation
EIRP (dBm)
Standard Deviation Measurement Diff (Hz)
R13OCT04
E - 3
3.0
Frequency Measurement Accuracy Test Results Measured by the UK's GEOLUT
Carrier Frequency Measurement Accuracy
-1.0
-0.8
-0.6
-0.4
-0.2
0.0
0.2
0.4
0.6
0.8
1.0
EIRP (dBm)
Average Frequency Measurement Difference (Hz)
Carrier Frequency Measurement Standard Deviation
0.0
0.2
0.4
0.6
0.8
1.0
1.2
1.4
1.6
1.8
2.0
EIRP (dBm)
Standard Deviation of Frequency Meassurements (Hz)
- END OF ANNEX E -
R13OCT04
E - 4
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R13OCT04
F - 1
ANNEX F
CAPACITY TEST RESULTS
1.0
Capacity Test Results Measured by France's GEOLUT
2.0
Capacity Test Results Measured by Spain's GEOLUT
- END OF ANNEX F -
- END OF DOCUMENT -
0.8
0.85
0.9
0.95
Number of Active Beacons
Probability
Valid Msg in 5 min
Valid Msg in 10 min
Valid Msg in 15 min
Confirmed Complete in
15 min
90.0%
91.0%
92.0%
93.0%
94.0%
95.0%
96.0%
97.0%
98.0%
99.0%
100.0%
Beacon Load
Percentage of Beacons
Within 5 Min
Within 10 Min
Within 15 Min
Conf-Comp within 15 Min
R13OCT04
F - 2
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Cospas-Sarsat Secretariat
1250 Rene-Levesque Blvd. West, Suite 4215, Montreal (Quebec) H3B 4W8 Canada
Telephone: +1 514 500 7999
Fax: +1 514 500 7996
Email: mail@cospas-sarsat.int
Website: http://www.cospas-sarsat.int