1
Introduction
1.1 As a global navigation satellite system compatible
with other navigation satellite systems worldwide, the BDS is a system independently
developed and operated by China and is comprised of three major components: space
constellation, ground control segment and user terminals. The space constellation
consists of five geosynchronous earth orbit (GEO) satellites and 27 medium-earth
orbit (MEO) satellites and three inclined geosynchronous satellite orbit (IGSO)
satellites. The GEO satellites are positioned at longitudes of 058.75° E, 080° E,
110.5° E, 140° E and 160° E, respectively. The MEO satellites are operating in an
orbit with an altitude of 21,500 km and an inclination of 55°, which are evenly
distributed in three orbital planes. The IGSO satellites are operating in an orbit
with an altitude of 36,000 km and an inclination of 55°, which are evenly
distributed in three inclined geosynchronous orbital planes. The subsatellite track
for the three IGSO satellites are coincided while the longitude of the intersection
point is at 118° E. This geometry ensures that a minimum of four satellites are
visible to users worldwide with a position dilution of precision (PDOP) ≤ 6. Each
satellite transmits open service signal B1I on "L" bands with carrier frequency as
1561.098 MHz. B1I signal includes ranging code which could provide the open service.
A navigation data message is superimposed on this code. BDS satellites are
identified by Code Division Multiple Access (CDMA).
1.2 The BDS Open Service (OS) provides positioning,
navigation and timing services, free of direct user charges. The BDS receiver
equipment should be capable of receiving and processing the open service signal.
1.3 BDS receiver equipment intended for navigational
purposes on ships with a speed not exceeding 70 knots, in addition to the general
requirements specified in 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 BDS
receiver.
2 BDS receiver equipment
2.1 The term "BDS 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 BDS receiver
equipment should include the following minimum facilities:
- .1 antenna capable of receiving
BDS signals;
- .2 BDS receiver and processor;
- .3 means of accessing the computed
latitude/longitude position;
- .4 data control and interface;
and
- .5 position display and, if
required, other forms of output.
If BDS forms part of an approved Integrated Navigation System (INS), requirements of
2.1.3, 2.1.4, 2.1.5 may be provided within the INS.
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 BDS receiver
equipment
The BDS receiver equipment should:
- .1 be capable of receiving and
processing the BDS positioning and velocity, and timing signals, and should
use the ionospheric model broadcast to the receiver by the constellation to
generate ionospheric corrections;
- .2 provide position information in
latitude and longitude in degrees, minutes and thousandths of minutesfootnote;
- .3 provide time referenced to
universal time coordinated UTC (NTSC)footnote;
- .4 be provided with at least two
outputs from which position information, UTC, course over ground (COG),
speed over ground (SOG) and alarms can be supplied to other equipment. The
output of position information should be based on the WGS 84 datum and
should be in accordance with international standardsfootnote. The output of UTC, course over
ground (COG), speed over ground (SOG) and alarms should be consistent with
the requirements of 3.15 and 3.17;
- .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%);
- .6 have dynamic accuracy equivalent
to the static accuracy specified in .5 above under the normal sea states and
motion experienced in shipsfootnote;
- .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;
- .8 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;
- .9 be capable of acquiring
satellite signals with input signals having carrier levels in the range of
-130dBm to -120dBm. Once the satellite signals have been acquired, the
equipment should continue to operate satisfactorily with satellite signals
having carrier levels down to -133dBm;
- .10 be capable of operating
satisfactorily under normal interference conditions consistent with the
requirements of resolution A.694(17);
- .11 be capable of acquiring
position, velocity and time to the required accuracy within 12 min where
there is no valid almanac data;
- .12 be capable of acquiring
position, velocity and time to the required accuracy within 1 min where
there is valid almanac data;
- .13 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;
- .14 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;
- .15 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;
- .16 provide at least one normally
closed contact, which should indicate failure of the BDS receiver
equipment;
- .17 have a bidirectional interface
to facilitate communication so that alarms can be transferred to external
systems and so that audible alarms from the BDS receiver can be acknowledged
from external systems; the interface should comply with the relevant
international standardsfootnote; and
- .18 have the facilities to process
differential BDS (DBDS) data fed to it in accordance with the standards of
ITU-Rfootnote and the appropriate RTCM standard
and provide indication of the reception of DBDS signals and whether they are
being applied to the ship's position. When a BDS 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 BDS receiver equipment should also indicate
whether the performance of BDS 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 resolution A.1046(27) or
appendix 2 to resolution A.915(22) and any subsequent amendments, as
appropriate.
4.2 The BDS receiver equipment should, as a
minimum
- .1 provide a warning within 5 s of
loss of position or if a new position based on the information provided by
the BDS 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;
- .2 use Receiver Autonomous
Integrity Monitoring (RAIM) to provide integrity performance appropriate to
the operation being undertaken; and
- .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 BDS receiver equipment inputs or outputs for a duration of
five minutes.