1 Introduction
1.1 IRNSS is a regional navigation satellite system compatible with other navigation
satellite systems worldwide. IRNSS is an independent regional system developed and
operated by India which comprises of three major components: space segment, ground
control segment and user terminals. The space segment is a constellation of seven
satellites, of which four are geosynchronous earth orbit (GSO) satellites inclined at
29° to equatorial plane with longitude crossing as 55°E and 111.75°E (two satellites in
each slot) and three are geostationary satellite orbit (GEO) satellites positioned at
32.5°E, 83°E, 129.5°E orbital slots. This geometry ensures that a minimum of five
satellites are visible to users within the service area with a position dilution of
precision (PDOP) ≤ 6. Each satellite transmits standard positioning service signals on
"L5" and "S" bands with carrier frequencies as 1176.45 MHz and 2492.028 MHz
respectively. Standard positioning signals include ranging codes which could provide the
open service. A navigation data message is superimposed on these codes. IRNSS satellites
are identified by pseudo ranging noise (PRN) codes.
1.2 The IRNSS Standard Positioning Service (SPS) provides positioning, navigation and
timing services, free of direct user charges. The IRNSS receiver equipment should be
capable of receiving and processing the standard service signal.
1.3 IRNSS receiver equipment intended for navigation purposes on ships with a speed not
exceeding 70 knots, in addition to the general requirements specified in the General
requirements for shipbore radio equipment forming part of the global maritime
distress and safety system (GMDSS) and for electronic navigational aids (resolution A.694(17)),footnote should comply with the following minimum performance
requirements.
1.4 The standards cover the basic requirements of position fixing, determination of
course over ground (COG), speed over ground (SOG) and timing, either for navigation
purposes or as input to other functions. The standards do not cover other computational
facilities which may be in the equipment nor cover the requirements for other systems
that may take input from the IRNSS receiver.
1.5 It should be noted that this is the regional navigation satellite system being
recognized as a future component of the World-Wide Radio Navigation System (WWRNS) and
the service is limited to the following coverage area.
2 IRNSS receiver equipment
2.1 The term "IRNSS receiver equipment" as used in the performance standards includes all
the components and units necessary for the system to properly perform its intended
functions. The IRNSS receiver equipment should include the following minimum facilities:
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.1 antenna capable of receiving IRNSS signals;
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.2 IRNSS receiver and processor;
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.3 means of accessing the computed latitude/longitude position;
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.4 data control and interface; and
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.5 position display and, if required, other forms of output.
2.2 The antenna design should be suitable for fitting at a position on the ship which
ensures a clear view of the satellite constellation, taking into consideration any
obstructions that might exist on the ship.
3 Performance standards for IRNSS receiver equipment
The IRNSS receiver equipment should:
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.1 be capable of receiving and processing the IRNSS positioning and velocity, and
timing signals, and should use the ionospheric model broadcast to the receiver
by the constellation to generate ionospheric corrections;
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.2 provide position information based upon WGS-84 coordinates and
should be in accordance with international standards;footnote
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.3 provide time referenced to universal time coordinated UTC;
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.4 be provided with at least two outputs from which position information, UTC,
COG, SOG and alarms can be supplied to other equipment. The output of UTC, COG,
SOG and alarms should be consistent with the requirements of 3.16 and 3.18;
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.5 have static accuracy such that the position of the antenna is determined to be
within 25 m horizontally (95%) and 30 m vertically (95%);
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.6 have dynamic accuracy equivalent to the static accuracy specified
in 3.5 above under the normal sea states and motion experienced in ships;footnote
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.7 have position information in latitude and longitude in degrees, minutes and
thousandths of minutes with a position resolution equal to or better than 0.001
min of latitude and longitude;
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.8 have timing accuracy such that time is determined within 100 ns of UTC;
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.9 be capable of selecting automatically the appropriate satellite-transmitted
signals to determine the ship's position and velocity, and time with the
required accuracy and update rate;
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.10 be capable of acquiring satellite signals with input signals having carrier
levels in the range of -137dBm to -127dBm. Once the satellite signals have been
acquired, the equipment should continue to operate satisfactorily with satellite
signals having carrier levels down to -140dBm;
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.11 be capable of operating satisfactorily under normal interference conditions
consistent with the requirements of resolution A.694(17);
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.12 be capable of acquiring position, velocity and time to the required accuracy
within 3 min where there is no valid almanac data;
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.13 be capable of acquiring position, velocity and time to the required accuracy
within 2 min where there is valid almanac data;
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.14 be capable of reacquiring position, velocity and time to the required
accuracy within 1 min when there has been a service interruption of 60 s or
less;
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.15 generate and output to a display and digital interfacefootnote a new position solution at least once every 1 s
for conventional craft and at least once every 0.5 s for high-speed craft;
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.16 provide the COG, SOG and UTC outputs, with a validity mark
aligned with that on the position output. The accuracy requirements for COG and
SOG should not be inferior to the relevant performance standards for
headingfootnote and speed and distance measuring equipment
(SDME)footnote and the accuracy should be obtained under the
various dynamic conditions that could be experienced on board ships;
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.17 provide at least one normally closed contact, which should indicate failure
of the IRNSS receiver equipment;
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.18 have a bidirectional interface to facilitate communication so
that alarms can be transferred to external systems and so that audible alarms
from the IRNSS receiver can be acknowledged from external systems; the interface
should comply with the relevant international standards;footnote and
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.19 have the facilities to process differential IRNSS (D-IRNSS) data
fed to it in accordance with the standards of ITU-Rfootnote and the appropriate RTCM standard and provide
indication of the reception of D-IRNSS signals and whether they are being
applied to the ship's position. When an IRNSS receiver is equipped with a
differential receiver, performance standards for static and dynamic accuracies
(paragraphs 3.5 and 3.6 above) should be 10 m (95%).
4 Integrity checking, failure warnings and status indications
4.1 The IRNSS receiver equipment should also indicate whether the
performance of IRNSS is outside the bounds of requirements for general navigation in the
ocean, coastal, port approach and restricted waters, and inland waterway phases of the
voyage as specified in either the Worldwide radionavigation system (resolution A.1046(27)) or appendix 2 to the Revised maritime policy and
requirements for a future global navigation satellite system (GNSS) (resolution
A.915(22)) and any subsequent amendments, as appropriate.
4.2 The IRNSS receiver equipment should, as a minimum:
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.1 provide a warning within 5 s of loss of position or if a new position based on
the information provided by the IRNSS constellation has not been calculated for
more than 1 s for conventional craft and 0.5 s for high-speed craft. Under such
conditions the last known position and the time of last valid fix, with the
explicit indication of the state allowing for no ambiguity, should be output
until normal operation is resumed;
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.2 use receiver autonomous integrity monitoring (RAIM) to provide integrity
performance appropriate to the operation being undertaken; and
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.3 provide a self-test function.
5 Protection
Precautions should be taken to ensure that no permanent damage can result from an
accidental short circuit or grounding of the antenna or any of its input or output
connections or any of the IRNSS receiver equipment inputs or outputs for a duration of 5
min.