GPSD_JSON(5) GPSD Documentation GPSD_JSON(5)NAMEgpsd_json - gpsd request/response protocol
OVERVIEW
gpsd is a service daemon that can be used to monitor GPSes, DGPS
receivers, Marine AIS broadcasts, and various other location-related
and kinematic sensors.
Clients may communicate with gpsd via textual requests and responses
over a socket. It is a bad idea for applications to speak the protocol
directly: rather, they should use the libgps client library (for C;
bindings also exist for other languages) and take appropriate care to
conditionalize their code on the major and minor protocol version
symbols.
The GPSD protocol is built on top of JSON, JavaScript Object Notation.
GPSD's use of JSON is restricted in some ways that make parsing it in
fixed-extent languages (such as C) easier.
A request line is introduced by "?" and may include multiple commands.
Commands begin with a command identifier, followed either by a
terminating ';' or by an equal sign "=" and a JSON object treated as an
argument. Any ';' or newline indication (either LF or CR-LF) after the
end of a command is ignored. All request lines must be composed of
US-ASCII characters and may be no more than 80 characters in length,
exclusive of the trailing newline.
Responses are JSON objects all of which have a "class" attribute the
value of which is either the name of the invoking command. There are
reports (including but not limited to as "TPV", "SKY", "DEVICE", and
"ERROR") which are not direct responses to commands.
The order of JSON attributes within a response object is never
significant, and you may specify attributes in commands in any order.
Responses never contain the special JSON value null; instead,
attributes with empty or undefined values are omitted. The length limit
for responses and reports is 1536 characters, including trailing
newline; longer responses will be truncated, so client code must be
prepared for the possibility of invalid JSON fragments.
In JSON reports, if an attribute is present only if the parent
attribute is present or has a particular range, then the parent
attribute is emitted first.
There is one constraint on the order in which attributes will be
omitted. If an optional attribute is present only when a parent
attribute has a specified value or range of values, the parent
attribute will be emitted first to make parsing easier.
The next subsection section documents the core GPSD protocol.
Extensions are documented in the following subsections. The extensions
may not be supported in your gpsd instance if it has been compiled with
a restricted feature set.
CORE SOCKET PROTOCOL
Here are the core-protocol responses:
TPV
A TPV object is a time-position-velocity report. The "class" and
"mode" fields will reliably be present. The "mode" field will be
emitted before optional fields that may be absent when there is no
fix. Error estimates will be emitted after the fix components
they're associated with. Others may be reported or not depending on
the fix quality.
Table 1. TPV object
┌───────┬─────────┬─────────┬──────────────────┐
│Name │ Always? │ Type │ Description │
├───────┼─────────┼─────────┼──────────────────┤
│class │ Yes │ string │ Fixed: "TPV" │
├───────┼─────────┼─────────┼──────────────────┤
│device │ No │ string │ Name of │
│ │ │ │ originating │
│ │ │ │ device. │
├───────┼─────────┼─────────┼──────────────────┤
│mode │ Yes │ numeric │ NMEA mode: %d, │
│ │ │ │ 0=no mode value │
│ │ │ │ yet seen, 1=no │
│ │ │ │ fix, 2=2D, 3=3D. │
├───────┼─────────┼─────────┼──────────────────┤
│time │ No │ string │ Time/date stamp │
│ │ │ │ in ISO8601 │
│ │ │ │ format, UTC. May │
│ │ │ │ have a │
│ │ │ │ fractional │
│ │ │ │ part of up to │
│ │ │ │ .001sec │
│ │ │ │ precision. May │
│ │ │ │ be absent if │
│ │ │ │ mode │
│ │ │ │ is not 2 │
│ │ │ │ or 3. │
├───────┼─────────┼─────────┼──────────────────┤
│ept │ No │ numeric │ Estimated │
│ │ │ │ timestamp error │
│ │ │ │ (%f, seconds, │
│ │ │ │ 95% confidence). │
│ │ │ │ Present │
│ │ │ │ if time is │
│ │ │ │ present. │
├───────┼─────────┼─────────┼──────────────────┤
│lat │ No │ numeric │ Latitude in │
│ │ │ │ degrees: +/- │
│ │ │ │ signifies │
│ │ │ │ North/South. │
│ │ │ │ Present │
│ │ │ │ when │
│ │ │ │ mode is 2 or 3. │
├───────┼─────────┼─────────┼──────────────────┤
│lon │ No │ numeric │ Longitude in │
│ │ │ │ degrees: +/- │
│ │ │ │ signifies │
│ │ │ │ East/West. │
│ │ │ │ Present │
│ │ │ │ when │
│ │ │ │ mode is 2 or 3. │
├───────┼─────────┼─────────┼──────────────────┤
│alt │ No │ numeric │ Altitude in │
│ │ │ │ meters. Present │
│ │ │ │ if mode is 3. │
├───────┼─────────┼─────────┼──────────────────┤
│epx │ No │ numeric │ Longitude error │
│ │ │ │ estimate in │
│ │ │ │ meters, 95% │
│ │ │ │ confidence. │
│ │ │ │ Present │
│ │ │ │ if mode │
│ │ │ │ is 2 or 3 and │
│ │ │ │ DOPs can be │
│ │ │ │ calculated from │
│ │ │ │ the satellite │
│ │ │ │ view. │
├───────┼─────────┼─────────┼──────────────────┤
│epy │ No │ numeric │ Latitude error │
│ │ │ │ estimate in │
│ │ │ │ meters, 95% │
│ │ │ │ confidence. │
│ │ │ │ Present │
│ │ │ │ if mode │
│ │ │ │ is 2 or 3 and │
│ │ │ │ DOPs can be │
│ │ │ │ calculated from │
│ │ │ │ the satellite │
│ │ │ │ view. │
├───────┼─────────┼─────────┼──────────────────┤
│epv │ No │ numeric │ Estimated │
│ │ │ │ vertical error │
│ │ │ │ in meters, 95% │
│ │ │ │ confidence. │
│ │ │ │ Present │
│ │ │ │ if mode │
│ │ │ │ is 3 and DOPs │
│ │ │ │ can be │
│ │ │ │ calculated from │
│ │ │ │ the satellite │
│ │ │ │ view. │
├───────┼─────────┼─────────┼──────────────────┤
│track │ No │ numeric │ Course over │
│ │ │ │ ground, degrees │
│ │ │ │ from true north. │
├───────┼─────────┼─────────┼──────────────────┤
│speed │ No │ numeric │ Speed over │
│ │ │ │ ground, meters │
│ │ │ │ per second. │
├───────┼─────────┼─────────┼──────────────────┤
│climb │ No │ numeric │ Climb (positive) │
│ │ │ │ or sink │
│ │ │ │ (negative) rate, │
│ │ │ │ meters per │
│ │ │ │ second. │
├───────┼─────────┼─────────┼──────────────────┤
│epd │ No │ numeric │ Direction error │
│ │ │ │ estimate in │
│ │ │ │ degrees, 95% │
│ │ │ │ confidence. │
├───────┼─────────┼─────────┼──────────────────┤
│eps │ No │ numeric │ Speed error │
│ │ │ │ estinmate in │
│ │ │ │ meters/sec, 95% │
│ │ │ │ confidence. │
├───────┼─────────┼─────────┼──────────────────┤
│epc │ No │ numeric │ Climb/sink error │
│ │ │ │ estimate in │
│ │ │ │ meters/sec, 95% │
│ │ │ │ confidence. │
└───────┴─────────┴─────────┴──────────────────┘
When the C client library parses a response of this kind, it will
assert validity bits in the top-level set member for each field
actually received; see gps.h for bitmask names and values.
Here's an example:
{"class":"TPV","device":"/dev/pts/1",
"time":"2005-06-08T10:34:48.283Z","ept":0.005,
"lat":46.498293369,"lon":7.567411672,"alt":1343.127,
"eph":36.000,"epv":32.321,
"track":10.3788,"speed":0.091,"climb":-0.085,"mode":3}
SKY
A SKY object reports a sky view of the GPS satellite positions. If
there is no GPS device available, or no skyview has been reported
yet, only the "class" field will reliably be present.
Table 2. SKY object
┌───────────┬─────────┬─────────┬──────────────────┐
│Name │ Always? │ Type │ Description │
├───────────┼─────────┼─────────┼──────────────────┤
│class │ Yes │ string │ Fixed: "SKY" │
├───────────┼─────────┼─────────┼──────────────────┤
│device │ No │ string │ Name of │
│ │ │ │ originating │
│ │ │ │ device │
├───────────┼─────────┼─────────┼──────────────────┤
│time │ No │ numeric │ Time/date stamp │
│ │ │ │ in ISO8601 │
│ │ │ │ format, UTC. May │
│ │ │ │ have a │
│ │ │ │ fractional │
│ │ │ │ part of up to │
│ │ │ │ .001sec │
│ │ │ │ precision. │
├───────────┼─────────┼─────────┼──────────────────┤
│xdop │ No │ numeric │ Longitudinal │
│ │ │ │ dilution of │
│ │ │ │ precision, a │
│ │ │ │ dimensionless │
│ │ │ │ factor │
│ │ │ │ which should be │
│ │ │ │ multiplied by a │
│ │ │ │ base UERE to get │
│ │ │ │ an error │
│ │ │ │ estimate. │
├───────────┼─────────┼─────────┼──────────────────┤
│ydop │ No │ numeric │ Latitudinal │
│ │ │ │ dilution of │
│ │ │ │ precision, a │
│ │ │ │ dimensionless │
│ │ │ │ factor │
│ │ │ │ which should be │
│ │ │ │ multiplied by a │
│ │ │ │ base UERE to get │
│ │ │ │ an error │
│ │ │ │ estimate. │
├───────────┼─────────┼─────────┼──────────────────┤
│vdop │ No │ numeric │ Altitude │
│ │ │ │ dilution of │
│ │ │ │ precision, a │
│ │ │ │ dimensionless │
│ │ │ │ factor │
│ │ │ │ which should be │
│ │ │ │ multiplied by a │
│ │ │ │ base UERE to get │
│ │ │ │ an error │
│ │ │ │ estimate. │
├───────────┼─────────┼─────────┼──────────────────┤
│tdop │ No │ numeric │ Time dilution of │
│ │ │ │ precision, a │
│ │ │ │ dimensionless │
│ │ │ │ factor │
│ │ │ │ which should be │
│ │ │ │ multiplied by a │
│ │ │ │ base UERE to get │
│ │ │ │ an error │
│ │ │ │ estimate. │
├───────────┼─────────┼─────────┼──────────────────┤
│hdop │ No │ numeric │ Horizontal │
│ │ │ │ dilution of │
│ │ │ │ precision, a │
│ │ │ │ dimensionless │
│ │ │ │ factor │
│ │ │ │ which should be │
│ │ │ │ multiplied by a │
│ │ │ │ base UERE to get │
│ │ │ │ a circular │
│ │ │ │ error estimate. │
├───────────┼─────────┼─────────┼──────────────────┤
│pdop │ No │ numeric │ Spherical │
│ │ │ │ dilution of │
│ │ │ │ precision, a │
│ │ │ │ dimensionless │
│ │ │ │ factor │
│ │ │ │ which should be │
│ │ │ │ multiplied by a │
│ │ │ │ base UERE to get │
│ │ │ │ an error │
│ │ │ │ estimate. │
├───────────┼─────────┼─────────┼──────────────────┤
│gdop │ No │ numeric │ Hyperspherical │
│ │ │ │ dilution of │
│ │ │ │ precision, a │
│ │ │ │ dimensionless │
│ │ │ │ factor │
│ │ │ │ which should be │
│ │ │ │ multiplied by a │
│ │ │ │ base UERE to get │
│ │ │ │ an error │
│ │ │ │ estimate. │
├───────────┼─────────┼─────────┼──────────────────┤
│satellites │ Yes │ list │ List of │
│ │ │ │ satellite │
│ │ │ │ objects in │
│ │ │ │ skyview │
└───────────┴─────────┴─────────┴──────────────────┘
Many devices compute dilution of precision factors but do not
include them in their reports. Many that do report DOPs report only
HDOP, two-dimensional circular error. gpsd always passes through
whatever the device actually reports, then attempts to fill in
other DOPs by calculating the appropriate determinants in a
covariance matrix based on the satellite view. DOPs may be missing
if some of these determinants are singular. It can even happen that
the device reports an error estimate in meters when the
corresponding DOP is unavailable; some devices use more
sophisticated error modeling than the covariance calculation.
The satellite list objects have the following elements:
Table 3. Satellite object
┌─────┬─────────┬─────────┬──────────────────┐
│Name │ Always? │ Type │ Description │
├─────┼─────────┼─────────┼──────────────────┤
│PRN │ Yes │ numeric │ PRN ID of the │
│ │ │ │ satellite. 1-63 │
│ │ │ │ are GNSS │
│ │ │ │ satellites, │
│ │ │ │ 64-96 are │
│ │ │ │ GLONASS │
│ │ │ │ satellites, │
│ │ │ │ 100-164 are SBAS │
│ │ │ │ satellites │
├─────┼─────────┼─────────┼──────────────────┤
│az │ Yes │ numeric │ Azimuth, degrees │
│ │ │ │ from true north. │
├─────┼─────────┼─────────┼──────────────────┤
│el │ Yes │ numeric │ Elevation in │
│ │ │ │ degrees. │
├─────┼─────────┼─────────┼──────────────────┤
│ss │ Yes │ numeric │ Signal strength │
│ │ │ │ in dB. │
├─────┼─────────┼─────────┼──────────────────┤
│used │ Yes │ boolean │ Used in current │
│ │ │ │ solution? │
│ │ │ │ (SBAS/WAAS/EGNOS │
│ │ │ │ satellites │
│ │ │ │ may be │
│ │ │ │ flagged used if │
│ │ │ │ the solution has │
│ │ │ │ corrections from │
│ │ │ │ them, but │
│ │ │ │ not all drivers │
│ │ │ │ make this │
│ │ │ │ information │
│ │ │ │ available.) │
└─────┴─────────┴─────────┴──────────────────┘
Note that satellite objects do not have a "class" field, as they
are never shipped outside of a SKY object.
When the C client library parses a SKY response, it will assert the
SATELLITE_SET bit in the top-level set member.
Here's an example:
{"class":"SKY","device":"/dev/pts/1",
"time":"2005-07-08T11:28:07.114Z",
"xdop":1.55,"hdop":1.24,"pdop":1.99,
"satellites":[
{"PRN":23,"el":6,"az":84,"ss":0,"used":false},
{"PRN":28,"el":7,"az":160,"ss":0,"used":false},
{"PRN":8,"el":66,"az":189,"ss":44,"used":true},
{"PRN":29,"el":13,"az":273,"ss":0,"used":false},
{"PRN":10,"el":51,"az":304,"ss":29,"used":true},
{"PRN":4,"el":15,"az":199,"ss":36,"used":true},
{"PRN":2,"el":34,"az":241,"ss":43,"used":true},
{"PRN":27,"el":71,"az":76,"ss":43,"used":true}]}
GST
A GST object is a pseudorange noise report.
Table 4. GST object
┌───────┬─────────┬─────────┬──────────────────┐
│Name │ Always? │ Type │ Description │
├───────┼─────────┼─────────┼──────────────────┤
│class │ Yes │ string │ Fixed: "GST" │
├───────┼─────────┼─────────┼──────────────────┤
│device │ No │ string │ Name of │
│ │ │ │ originating │
│ │ │ │ device │
├───────┼─────────┼─────────┼──────────────────┤
│time │ No │ numeric │ Seconds since │
│ │ │ │ the Unix epoch, │
│ │ │ │ UTC. May have a │
│ │ │ │ fractional part │
│ │ │ │ of up to .001sec │
│ │ │ │ precision. │
├───────┼─────────┼─────────┼──────────────────┤
│rms │ No │ numeric │ Value of the │
│ │ │ │ standard │
│ │ │ │ deviation of the │
│ │ │ │ range inputs to │
│ │ │ │ the navigation │
│ │ │ │ process (range │
│ │ │ │ inputs include │
│ │ │ │ pseudoranges and │
│ │ │ │ DGPS │
│ │ │ │ corrections). │
├───────┼─────────┼─────────┼──────────────────┤
│major │ No │ numeric │ Standard │
│ │ │ │ deviation of │
│ │ │ │ semi-major axis │
│ │ │ │ of error │
│ │ │ │ ellipse, in │
│ │ │ │ meters. │
├───────┼─────────┼─────────┼──────────────────┤
│minor │ No │ numeric │ Standard │
│ │ │ │ deviation of │
│ │ │ │ semi-minor axis │
│ │ │ │ of error │
│ │ │ │ ellipse, in │
│ │ │ │ meters. │
├───────┼─────────┼─────────┼──────────────────┤
│orient │ No │ numeric │ Orientation of │
│ │ │ │ semi-major axis │
│ │ │ │ of error │
│ │ │ │ ellipse, in │
│ │ │ │ degrees from │
│ │ │ │ true north. │
├───────┼─────────┼─────────┼──────────────────┤
│lat │ No │ numeric │ Standard │
│ │ │ │ deviation of │
│ │ │ │ latitude error, │
│ │ │ │ in meters. │
├───────┼─────────┼─────────┼──────────────────┤
│lon │ No │ numeric │ Standard │
│ │ │ │ deviation of │
│ │ │ │ longitude error, │
│ │ │ │ in meters. │
├───────┼─────────┼─────────┼──────────────────┤
│alt │ No │ numeric │ Standard │
│ │ │ │ deviation of │
│ │ │ │ altitude error, │
│ │ │ │ in meters. │
└───────┴─────────┴─────────┴──────────────────┘
Here's an example:
{"class":"GST","device":"/dev/ttyUSB0",
"time":"2010-12-07T10:23:07.096Z","rms":2.440,
"major":1.660,"minor":1.120,"orient":68.989,
"lat":1.600,"lon":1.200,"alt":2.520}
ATT
An ATT object is a vehicle-attitude report. It is returned by
digital-compass and gyroscope sensors; depending on device, it may
include: heading, pitch, roll, yaw, gyroscope, and magnetic-field
readings. Because such sensors are often bundled as part of
marine-navigation systems, the ATT response may also include water
depth.
The "class" and "mode" fields will reliably be present. Others may
be reported or not depending on the specific device type.
Table 5. ATT object
┌────────────┬─────────┬─────────┬──────────────────┐
│Name │ Always? │ Type │ Description │
├────────────┼─────────┼─────────┼──────────────────┤
│class │ Yes │ string │ Fixed: "ATT" │
├────────────┼─────────┼─────────┼──────────────────┤
│device │ Yes │ string │ Name of │
│ │ │ │ originating │
│ │ │ │ device │
├────────────┼─────────┼─────────┼──────────────────┤
│time │ Yes │ numeric │ Seconds since │
│ │ │ │ the Unix epoch, │
│ │ │ │ UTC. May have a │
│ │ │ │ fractional │
│ │ │ │ part of up to │
│ │ │ │ .001sec │
│ │ │ │ precision. │
├────────────┼─────────┼─────────┼──────────────────┤
│heading │ No │ numeric │ Heading, degrees │
│ │ │ │ from true north. │
├────────────┼─────────┼─────────┼──────────────────┤
│mag_st │ No │ string │ Magnetometer │
│ │ │ │ status. │
├────────────┼─────────┼─────────┼──────────────────┤
│pitch │ No │ numeric │ Pitch in │
│ │ │ │ degrees. │
├────────────┼─────────┼─────────┼──────────────────┤
│pitch_st │ No │ string │ Pitch sensor │
│ │ │ │ status. │
├────────────┼─────────┼─────────┼──────────────────┤
│yaw │ No │ numeric │ Yaw in degrees │
├────────────┼─────────┼─────────┼──────────────────┤
│yaw_st │ No │ string │ Yaw sensor │
│ │ │ │ status. │
├────────────┼─────────┼─────────┼──────────────────┤
│roll │ No │ numeric │ Roll in degrees. │
├────────────┼─────────┼─────────┼──────────────────┤
│roll_st │ No │ string │ Roll sensor │
│ │ │ │ status. │
├────────────┼─────────┼─────────┼──────────────────┤
│dip │ No │ numeric │ Local magnetic │
│ │ │ │ inclination, │
│ │ │ │ degrees, │
│ │ │ │ positive when │
│ │ │ │ the magnetic │
│ │ │ │ field points │
│ │ │ │ downward (into │
│ │ │ │ the Earth). │
├────────────┼─────────┼─────────┼──────────────────┤
│mag_len │ No │ numeric │ Scalar magnetic │
│ │ │ │ field strength. │
├────────────┼─────────┼─────────┼──────────────────┤
│mag_x │ No │ numeric │ X component of │
│ │ │ │ magnetic field │
│ │ │ │ strength. │
├────────────┼─────────┼─────────┼──────────────────┤
│mag_y │ No │ numeric │ Y component of │
│ │ │ │ magnetic field │
│ │ │ │ strength. │
├────────────┼─────────┼─────────┼──────────────────┤
│mag_z │ No │ numeric │ Z component of │
│ │ │ │ magnetic field │
│ │ │ │ strength. │
├────────────┼─────────┼─────────┼──────────────────┤
│acc_len │ No │ numeric │ Scalar │
│ │ │ │ acceleration. │
├────────────┼─────────┼─────────┼──────────────────┤
│acc_x │ No │ numeric │ X component of │
│ │ │ │ acceleration. │
├────────────┼─────────┼─────────┼──────────────────┤
│acc_y │ No │ numeric │ Y component of │
│ │ │ │ acceleration. │
├────────────┼─────────┼─────────┼──────────────────┤
│acc_z │ No │ numeric │ Z component of │
│ │ │ │ acceleration. │
├────────────┼─────────┼─────────┼──────────────────┤
│gyro_x │ No │ numeric │ X component of │
│ │ │ │ acceleration. │
├────────────┼─────────┼─────────┼──────────────────┤
│gyro_y │ No │ numeric │ Y component of │
│ │ │ │ acceleration. │
├────────────┼─────────┼─────────┼──────────────────┤
│depth │ No │ numeric │ Water depth in │
│ │ │ │ meters. │
├────────────┼─────────┼─────────┼──────────────────┤
│temperature │ No │ numeric │ Temperature at │
│ │ │ │ sensor, degrees │
│ │ │ │ centigrade. │
└────────────┴─────────┴─────────┴──────────────────┘
The heading, pitch, and roll status codes (if present) vary by
device. For the TNT Revolution digital compasses, they are coded as
follows:
Table 6. Device flags
┌─────┬────────────────────────────┐
│Code │ Description │
├─────┼────────────────────────────┤
│C │ magnetometer calibration │
│ │ alarm │
├─────┼────────────────────────────┤
│L │ low alarm │
├─────┼────────────────────────────┤
│M │ low warning │
├─────┼────────────────────────────┤
│N │ normal │
├─────┼────────────────────────────┤
│O │ high warning │
├─────┼────────────────────────────┤
│P │ high alarm │
├─────┼────────────────────────────┤
│V │ magnetometer voltage level │
│ │ alarm │
└─────┴────────────────────────────┘
When the C client library parses a response of this kind, it will
assert ATT_IS.
Here's an example:
{"class":"ATT","time":1270938096.843,
"heading":14223.00,"mag_st":"N",
"pitch":169.00,"pitch_st":"N", "roll":-43.00,"roll_st":"N",
"dip":13641.000,"mag_x":2454.000}
And here are the commands:
?VERSION;
Returns an object with the following attributes:
Table 7. VERSION object
┌────────────┬─────────┬─────────┬──────────────────┐
│Name │ Always? │ Type │ Description │
├────────────┼─────────┼─────────┼──────────────────┤
│class │ Yes │ string │ Fixed: "VERSION" │
├────────────┼─────────┼─────────┼──────────────────┤
│release │ Yes │ string │ Public release │
│ │ │ │ level │
├────────────┼─────────┼─────────┼──────────────────┤
│rev │ Yes │ string │ Internal │
│ │ │ │ revision-control │
│ │ │ │ level. │
├────────────┼─────────┼─────────┼──────────────────┤
│proto_major │ Yes │ numeric │ API major │
│ │ │ │ revision level. │
├────────────┼─────────┼─────────┼──────────────────┤
│proto_minor │ Yes │ numeric │ API minor │
│ │ │ │ revision level. │
├────────────┼─────────┼─────────┼──────────────────┤
│remote │ No │ string │ URL of the │
│ │ │ │ remote daemon │
│ │ │ │ reporting this │
│ │ │ │ version. If │
│ │ │ │ empty, │
│ │ │ │ this is the │
│ │ │ │ version of the │
│ │ │ │ local daemon. │
└────────────┴─────────┴─────────┴──────────────────┘
The daemon ships a VERSION response to each client when the client
first connects to it.
When the C client library parses a response of this kind, it will
assert the VERSION_SET bit in the top-level set member.
Here's an example:
{"class":"VERSION","version":"2.40dev",
"rev":"06f62e14eae9886cde907dae61c124c53eb1101f",
"proto_major":3,"proto_minor":1
}
?DEVICES;
Returns a device list object with the following elements:
Table 8. DEVICES object
┌────────┬─────────┬────────┬──────────────────┐
│Name │ Always? │ Type │ Description │
├────────┼─────────┼────────┼──────────────────┤
│class │ Yes │ string │ Fixed: "DEVICES" │
├────────┼─────────┼────────┼──────────────────┤
│devices │ Yes │ list │ List of device │
│ │ │ │ descriptions │
├────────┼─────────┼────────┼──────────────────┤
│remote │ No │ string │ URL of the │
│ │ │ │ remote daemon │
│ │ │ │ reporting the │
│ │ │ │ device set. If │
│ │ │ │ empty, │
│ │ │ │ this is a │
│ │ │ │ DEVICES response │
│ │ │ │ from the local │
│ │ │ │ daemon. │
└────────┴─────────┴────────┴──────────────────┘
When the C client library parses a response of this kind, it will
assert the DEVICELIST_SET bit in the top-level set member.
Here's an example:
{"class"="DEVICES","devices":[
{"class":"DEVICE","path":"/dev/pts/1","flags":1,"driver":"SiRF binary"},
{"class":"DEVICE","path":"/dev/pts/3","flags":4,"driver":"AIVDM"}]}
The daemon occasionally ships a bare DEVICE object to the client
(that is, one not inside a DEVICES wrapper). The data content of
these objects will be described later as a response to the ?DEVICE
command.
?WATCH;
This command sets watcher mode. It also sets or elicits a report of
per-subscriber policy and the raw bit. An argument WATCH object
changes the subscriber's policy. The response describes the
subscriber's policy. The response will also include a DEVICES
object.
A WATCH object has the following elements:
Table 9. WATCH object
┌────────┬─────────┬─────────┬──────────────────┐
│Name │ Always? │ Type │ Description │
├────────┼─────────┼─────────┼──────────────────┤
│class │ Yes │ string │ Fixed: "WATCH" │
├────────┼─────────┼─────────┼──────────────────┤
│enable │ No │ boolean │ Enable (true) or │
│ │ │ │ disable (false) │
│ │ │ │ watcher mode. │
│ │ │ │ Default is │
│ │ │ │ true. │
├────────┼─────────┼─────────┼──────────────────┤
│json │ No │ boolean │ Enable (true) or │
│ │ │ │ disable (false) │
│ │ │ │ dumping of JSON │
│ │ │ │ reports. │
│ │ │ │ Default is │
│ │ │ │ false. │
├────────┼─────────┼─────────┼──────────────────┤
│nmea │ No │ boolean │ Enable (true) or │
│ │ │ │ disable (false) │
│ │ │ │ dumping of │
│ │ │ │ binary │
│ │ │ │ packets as │
│ │ │ │ pseudo-NMEA. │
│ │ │ │ Default is │
│ │ │ │ false. │
├────────┼─────────┼─────────┼──────────────────┤
│raw │ No │ integer │ Controls 'raw' │
│ │ │ │ mode. When this │
│ │ │ │ attribute is set │
│ │ │ │ to 1 for a │
│ │ │ │ channel, gpsd │
│ │ │ │ reports the │
│ │ │ │ unprocessed │
│ │ │ │ NMEA or AIVDM │
│ │ │ │ data stream from │
│ │ │ │ whatever device │
│ │ │ │ is attached. │
│ │ │ │ Binary GPS │
│ │ │ │ packets are │
│ │ │ │ hex-dumped. │
│ │ │ │ RTCM2 and RTCM3 │
│ │ │ │ packets │
│ │ │ │ are not dumped │
│ │ │ │ in raw mode. │
│ │ │ │ When this │
│ │ │ │ attribute is set │
│ │ │ │ to 2 for a │
│ │ │ │ channel that │
│ │ │ │ processes binary │
│ │ │ │ data, gpsd │
│ │ │ │ reports the │
│ │ │ │ received data │
│ │ │ │ verbatim │
│ │ │ │ without │
│ │ │ │ hex-dumping. │
├────────┼─────────┼─────────┼──────────────────┤
│scaled │ No │ boolean │ If true, apply │
│ │ │ │ scaling divisors │
│ │ │ │ to output before │
│ │ │ │ dumping; │
│ │ │ │ default is │
│ │ │ │ false. │
├────────┼─────────┼─────────┼──────────────────┤
│split24 │ No │ boolean │ If true, │
│ │ │ │ aggregate AIS │
│ │ │ │ type24 sentence │
│ │ │ │ parts. If │
│ │ │ │ false, │
│ │ │ │ report │
│ │ │ │ each part as a │
│ │ │ │ separate JSON │
│ │ │ │ object, leaving │
│ │ │ │ the │
│ │ │ │ client │
│ │ │ │ to match MMSIs │
│ │ │ │ and aggregate. │
│ │ │ │ Default is │
│ │ │ │ false. │
│ │ │ │ Applies only to │
│ │ │ │ AIS reports. │
├────────┼─────────┼─────────┼──────────────────┤
│pps │ No │ boolean │ If true, emit │
│ │ │ │ the TOFF JSON │
│ │ │ │ message on each │
│ │ │ │ cycle and a │
│ │ │ │ PPS JSON │
│ │ │ │ message when the │
│ │ │ │ device issues │
│ │ │ │ 1PPS. Default is │
│ │ │ │ false. │
├────────┼─────────┼─────────┼──────────────────┤
│device │ No │ string │ If present, │
│ │ │ │ enable watching │
│ │ │ │ only of the │
│ │ │ │ specified device │
│ │ │ │ rather than │
│ │ │ │ all devices. │
│ │ │ │ Useful with raw │
│ │ │ │ and NMEA modes │
│ │ │ │ in which │
│ │ │ │ device responses │
│ │ │ │ aren't tagged. │
│ │ │ │ Has no effect │
│ │ │ │ when used │
│ │ │ │ with │
│ │ │ │ enable:false. │
├────────┼─────────┼─────────┼──────────────────┤
│remote │ No │ string │ URL of the │
│ │ │ │ remote daemon │
│ │ │ │ reporting the │
│ │ │ │ watch set. If │
│ │ │ │ empty, │
│ │ │ │ this is a WATCH │
│ │ │ │ response from │
│ │ │ │ the local │
│ │ │ │ daemon. │
└────────┴─────────┴─────────┴──────────────────┘
There is an additional boolean "timing" attribute which is
undocumented because that portion of the interface is considered
unstable and for developer use only.
In watcher mode, GPS reports are dumped as TPV and SKY responses.
AIS, Subframe and RTCM reporting is described in the next section.
When the C client library parses a response of this kind, it will
assert the POLICY_SET bit in the top-level set member.
Here's an example:
{"class":"WATCH", "raw":1,"scaled":true}
?POLL;
The POLL command requests data from the last-seen fixes on all
active GPS devices. Devices must previously have been activated by
?WATCH to be pollable.
Polling can lead to possibly surprising results when it is used on
a device such as an NMEA GPS for which a complete fix has to be
accumulated from several sentences. If you poll while those
sentences are being emitted, the response will contain the last
complete fix data and may be as much as one cycle time (typically 1
second) stale.
The POLL response will contain a timestamped list of TPV objects
describing cached data, and a timestamped list of SKY objects
describing satellite configuration. If a device has not seen fixes,
it will be reported with a mode field of zero.
Table 10. POLL object
┌─────────┬─────────┬────────────┬──────────────────┐
│Name │ Always? │ Type │ Description │
├─────────┼─────────┼────────────┼──────────────────┤
│class │ Yes │ string │ Fixed: "POLL" │
├─────────┼─────────┼────────────┼──────────────────┤
│time │ Yes │ Numeric │ Timestamp in ISO │
│ │ │ │ 8601 format. May │
│ │ │ │ have a │
│ │ │ │ fractional │
│ │ │ │ part of up to │
│ │ │ │ .001sec │
│ │ │ │ precision. │
├─────────┼─────────┼────────────┼──────────────────┤
│active │ Yes │ Numeric │ Count of active │
│ │ │ │ devices. │
├─────────┼─────────┼────────────┼──────────────────┤
│fixes │ Yes │ JSON array │ Comma-separated │
│ │ │ │ list of TPV │
│ │ │ │ objects. │
├─────────┼─────────┼────────────┼──────────────────┤
│skyviews │ Yes │ JSON array │ Comma-separated │
│ │ │ │ list of SKY │
│ │ │ │ objects. │
└─────────┴─────────┴────────────┴──────────────────┘
Here's an example of a POLL response:
{"class":"POLL","time":"2010-06-04T10:31:00.289Z","active":1,
"tpv":[{"class":"TPV","device":"/dev/ttyUSB0",
"time":"2010-09-08T13:33:06.095Z",
"ept":0.005,"lat":40.035093060,
"lon":-75.519748733,"track":99.4319,"speed":0.123,"mode":2}],
"sky":[{"class":"SKY","device":"/dev/ttyUSB0",
"time":1270517264.240,"hdop":9.20,
"satellites":[{"PRN":16,"el":55,"az":42,"ss":36,"used":true},
{"PRN":19,"el":25,"az":177,"ss":0,"used":false},
{"PRN":7,"el":13,"az":295,"ss":0,"used":false},
{"PRN":6,"el":56,"az":135,"ss":32,"used":true},
{"PRN":13,"el":47,"az":304,"ss":0,"used":false},
{"PRN":23,"el":66,"az":259,"ss":0,"used":false},
{"PRN":20,"el":7,"az":226,"ss":0,"used":false},
{"PRN":3,"el":52,"az":163,"ss":32,"used":true},
{"PRN":31,"el":16,"az":102,"ss":0,"used":false}
]}]}
Note
Client software should not assume the field inventory of the
POLL response is fixed for all time. As gpsd collects and
caches more data from more sensor types, those data are likely
to find their way into this response.
TOFF
This message is emitted on each cycle and reports the offset
between the host's clock time and the GPS time at top of second
(actually, when the first data for the reporting cycle is
received).
A TOFF object has the following elements:
Table 11. TOFF object
┌───────────┬─────────┬─────────┬──────────────────┐
│Name │ Always? │ Type │ Description │
├───────────┼─────────┼─────────┼──────────────────┤
│class │ Yes │ string │ Fixed: "TOFF" │
├───────────┼─────────┼─────────┼──────────────────┤
│device │ Yes │ string │ Name of │
│ │ │ │ originating │
│ │ │ │ device │
├───────────┼─────────┼─────────┼──────────────────┤
│real_sec │ Yes │ numeric │ seconds from the │
│ │ │ │ GPS clock │
├───────────┼─────────┼─────────┼──────────────────┤
│real_nsec │ Yes │ numeric │ nanoseconds from │
│ │ │ │ the GPS clock │
├───────────┼─────────┼─────────┼──────────────────┤
│clock_sec │ Yes │ numeric │ seconds from the │
│ │ │ │ system clock │
├───────────┼─────────┼─────────┼──────────────────┤
│clock_nsec │ Yes │ numeric │ nanoseconds from │
│ │ │ │ the system clock │
└───────────┴─────────┴─────────┴──────────────────┘
This message is emitted once per second to watchers of a device and
is intended to report the offset between the in-band report of the
GPS and seconds as reported by the system clock (which may be
NTP-corrected) when the first valid timestamp of the reporting
cycle is seen.
The message contains second/microsecond pairs for two clocks; the
realtime clock without NTP correction (the result of
clock_gettime(CLOCK_REALTIME), but only to microsecond precision)
and the ordinary system clock (which may be NTP corrected).
Here's an example:
{"class":"TOFF","device":"/dev/ttyUSB0",
"real_sec":1330212592, "real_nsec":343182,
"clock_sec":1330212592,"clock_nsec":343184}
PPS
This message is emitted each time the daemon sees a PPS (Pulse Per
Second) strobe from a device.
A PPS object has the following elements:
Table 12. PPS object
┌───────────┬─────────┬─────────┬──────────────────┐
│Name │ Always? │ Type │ Description │
├───────────┼─────────┼─────────┼──────────────────┤
│class │ Yes │ string │ Fixed: "PPS" │
├───────────┼─────────┼─────────┼──────────────────┤
│device │ Yes │ string │ Name of │
│ │ │ │ originating │
│ │ │ │ device │
├───────────┼─────────┼─────────┼──────────────────┤
│real_sec │ Yes │ numeric │ seconds from the │
│ │ │ │ realtime clock │
├───────────┼─────────┼─────────┼──────────────────┤
│real_nsec │ Yes │ numeric │ nanoseconds from │
│ │ │ │ the realtime │
│ │ │ │ clock │
├───────────┼─────────┼─────────┼──────────────────┤
│clock_sec │ Yes │ numeric │ seconds from the │
│ │ │ │ system clock │
├───────────┼─────────┼─────────┼──────────────────┤
│clock_nsec │ Yes │ numeric │ nanoseconds from │
│ │ │ │ the system clock │
└───────────┴─────────┴─────────┴──────────────────┘
This message is emitted once per second to watchers of a device
emitting PPS, and is intended to report the offset between the
start of the GPS second (when the 1PPS arrives) and seconds as
reported by the system clock (which may be NTP-corrected).
The message contains second/microsecond pairs for two clocks; the
realtime clock without NTP correction (the result of
clock_gettime(CLOCK_REALTIME), but only to microsecond precision)
and the ordinary system clock (which may be NTP corrected).
There are various sources of error in the reported clock times. For
PPS delivered via a real serial-line strobe, serial-interrupt
latency plus processing time to the timer call should be bounded
above by about 10 microseconds; USB-to-serial control-line
emulation is known to add jitter of about 50 microseconds. (Both
figures are for GPSD running in non-realtime mode on an x86 with a
gigahertz clock and are estimates based on measured latency in
other applications.)
Here's an example:
{"class":"PPS","device":"/dev/ttyUSB0",
"real_sec":1330212592, "real_nsec":343182,
"clock_sec":1330212592,"clock_nsec":343184}
?DEVICE
This command reports (when followed by ';') the state of a device,
or sets (when followed by '=' and a DEVICE object) device-specific
control bits, notably the device's speed and serial mode and the
native-mode bit. The parameter-setting form will be rejected if
more than one client is attached to the channel.
Pay attention to the response, because it is possible for this
command to fail if the GPS does not support a speed-switching
command or only supports some combinations of serial modes. In case
of failure, the daemon and GPS will continue to communicate at the
old speed.
Use the parameter-setting form with caution. On USB and Bluetooth
GPSes it is also possible for serial mode setting to fail either
because the serial adaptor chip does not support non-8N1 modes or
because the device firmware does not properly synchronize the
serial adaptor chip with the UART on the GPS chipset when the speed
changes. These failures can hang your device, possibly requiring a
GPS power cycle or (in extreme cases) physically disconnecting the
NVRAM backup battery.
A DEVICE object has the following elements:
Table 13. CONFIGCHAN object
┌──────────┬──────────────────┬─────────┬────────────────────┐
│Name │ Always? │ Type │ Description │
├──────────┼──────────────────┼─────────┼────────────────────┤
│class │ Yes │ string │ Fixed: "DEVICE" │
├──────────┼──────────────────┼─────────┼────────────────────┤
│path │ No │ string │ Name the device │
│ │ │ │ for which the │
│ │ │ │ control bits are │
│ │ │ │ being │
│ │ │ │ reported, or for │
│ │ │ │ which they are │
│ │ │ │ to be applied. │
│ │ │ │ This │
│ │ │ │ attribute │
│ │ │ │ may be omitted │
│ │ │ │ only when there │
│ │ │ │ is exactly one │
│ │ │ │ subscribed │
│ │ │ │ channel. │
├──────────┼──────────────────┼─────────┼────────────────────┤
│activated │ No │ string │ Time the device │
│ │ │ │ was activated as │
│ │ │ │ an ISO8601 │
│ │ │ │ timestamp. │
│ │ │ │ If the device is │
│ │ │ │ inactive this │
│ │ │ │ attribute is │
│ │ │ │ absent. │
├──────────┼──────────────────┼─────────┼────────────────────┤
│flags │ No │ integer │ Bit vector of │
│ │ │ │ property flags. │
│ │ │ │ Currently defined │
│ │ │ │ flags are: │
│ │ │ │ describe │
│ │ │ │ packet types seen │
│ │ │ │ so far (GPS, │
│ │ │ │ RTCM2, RTCM3, │
│ │ │ │ AIS). Won't │
│ │ │ │ be reported if │
│ │ │ │ empty, e.g. before │
│ │ │ │ gpsd has seen │
│ │ │ │ identifiable │
│ │ │ │ packets from │
│ │ │ │ the device. │
├──────────┼──────────────────┼─────────┼────────────────────┤
│driver │ No │ string │ GPSD's name for │
│ │ │ │ the device driver │
│ │ │ │ type. Won't be │
│ │ │ │ reported before │
│ │ │ │ gpsd has seen │
│ │ │ │ identifiable │
│ │ │ │ packets from │
│ │ │ │ the device. │
├──────────┼──────────────────┼─────────┼────────────────────┤
│subtype │ When the daemon │ string │ Whatever version │
│ │ sees a delayed │ │ information the │
│ │ response to a │ │ device returned. │
│ │ probe for │ │ │
│ │ subtype or │ │ │
│ │ firmware-version │ │ │
│ │ information. │ │ │
├──────────┼──────────────────┼─────────┼────────────────────┤
│bps │ No │ integer │ Device speed in │
│ │ │ │ bits per second. │
├──────────┼──────────────────┼─────────┼────────────────────┤
│parity │ Yes │ string │ N, O or E for no │
│ │ │ │ parity, odd, or │
│ │ │ │ even. │
├──────────┼──────────────────┼─────────┼────────────────────┤
│stopbits │ Yes │ string │ Stop bits (1 or │
│ │ │ │ 2). │
├──────────┼──────────────────┼─────────┼────────────────────┤
│native │ No │ integer │ 0 means NMEA mode │
│ │ │ │ and 1 means │
│ │ │ │ alternate │
│ │ │ │ mode (binary if it │
│ │ │ │ has one, for SiRF │
│ │ │ │ and Evermore │
│ │ │ │ chipsets in │
│ │ │ │ particular). │
│ │ │ │ Attempting to set │
│ │ │ │ this mode on a │
│ │ │ │ non-GPS │
│ │ │ │ device will │
│ │ │ │ yield an error. │
├──────────┼──────────────────┼─────────┼────────────────────┤
│cycle │ No │ real │ Device cycle time │
│ │ │ │ in seconds. │
├──────────┼──────────────────┼─────────┼────────────────────┤
│mincycle │ No │ real │ Device minimum │
│ │ │ │ cycle time in │
│ │ │ │ seconds. Reported │
│ │ │ │ from │
│ │ │ │ ?CONFIGDEV │
│ │ │ │ when (and only │
│ │ │ │ when) the rate is │
│ │ │ │ switchable. It is │
│ │ │ │ read-only and │
│ │ │ │ not settable. │
└──────────┴──────────────────┴─────────┴────────────────────┘
The serial parameters will be omitted in a response describing a
TCP/IP source such as an Ntrip, DGPSIP, or AIS feed.
The contents of the flags field should be interpreted as follows:
Table 14. Device flags
┌───────────┬───────┬─────────────────────┐
│C #define │ Value │ Description │
├───────────┼───────┼─────────────────────┤
│SEEN_GPS │ 0x01 │ GPS data has been │
│ │ │ seen on this device │
├───────────┼───────┼─────────────────────┤
│SEEN_RTCM2 │ 0x02 │ RTCM2 data has been │
│ │ │ seen on this device │
├───────────┼───────┼─────────────────────┤
│SEEN_RTCM3 │ 0x04 │ RTCM3 data has been │
│ │ │ seen on this device │
├───────────┼───────┼─────────────────────┤
│SEEN_AIS │ 0x08 │ AIS data has been │
│ │ │ seen on this device │
└───────────┴───────┴─────────────────────┘
When the C client library parses a response of this kind, it will
assert the DEVICE_SET bit in the top-level set member.
Here's an example:
{"class":"DEVICE","bps":4800,"parity":"N","stopbits":1,"native":0}
When a client is in watcher mode, the daemon will ship it DEVICE
notifications when a device is added to the pool or deactivated.
When the C client library parses a response of this kind, it will
assert the DEVICE_SET bit in the top-level set member.
Here's an example:
{"class":"DEVICE","path":"/dev/pts1","activated":0}
The daemon may ship an error object in response to a syntactically
invalid command line or unknown command. It has the following elements:
Table 15. ERROR notification object
┌────────┬─────────┬────────┬────────────────┐
│Name │ Always? │ Type │ Description │
├────────┼─────────┼────────┼────────────────┤
│class │ Yes │ string │ Fixed: "ERROR" │
├────────┼─────────┼────────┼────────────────┤
│message │ Yes │ string │ Textual error │
│ │ │ │ message │
└────────┴─────────┴────────┴────────────────┘
Here's an example:
{"class":"ERROR","message":"Unrecognized request '?FOO'"}
When the C client library parses a response of this kind, it will
assert the ERR_SET bit in the top-level set member.
RTCM2
RTCM-104 is a family of serial protocols used for broadcasting
pseudorange corrections from differential-GPS reference stations. Many
GPS receivers can accept these corrections to improve their reporting
accuracy.
RTCM-104 comes in two major and incompatible flavors, 2.x and 3.x. Each
major flavor has minor (compatible) revisions.
The applicable standard for RTCM Version 2.x is RTCM Recommended
Standards for Differential NAVSTAR GPS Service RTCM Paper 194-93/SC
104-STD. For RTCM 3.1 it is RTCM Paper 177-2006-SC104-STD. Ordering
instructions for both standards are accessible from the website of the
Radio Technical Commission for Maritime Services[1] under
"Publications".
RTCM WIRE TRANSMISSIONS
Differential-GPS correction stations consist of a GPS reference
receiver coupled to a low frequency (LF) transmitter. The GPS reference
receiver is a survey-grade GPS that does GPS carrier tracking and can
work out its own position to a few millimeters. It generates range and
range-rate corrections and encodes them into RTCM104. It ships the
RTCM104 to the LF transmitter over serial rs-232 signal at 100 baud or
200 baud depending on the requirements of the transmitter.
The LF transmitter broadcasts the approximately 300khz radio signal
that differential-GPS radio receivers pick up. Transmitters that are
meant to have a higher range will need to transmit at the slower rate.
The higher the data rate the harder it will be for the remote radio
receiver to receive with a good signal-to-noise ration. (Higher data
rate signals can't be averaged over as long a time frame, hence they
appear noisier.)
RTCM WIRE FORMATS
An RTCM 2.x message consists of a sequence of up to 33 30-bit words.
The 24 most significant bits of each word are data and the six least
significant bits are parity. The parity algorithm used is the same
ISGPS-2000 as that used on GPS satellite downlinks. Each RTCM 2.x
message consists of two header words followed by zero or more data
words, depending upon message type.
An RTCM 3.x message begins with a fixed leader byte 0xD3. That is
followed by six bits of version information and 10 bits of payload
length information. Following that is the payload; following the
payload is a 3-byte checksum of the payload using the Qualcomm CRC-24Q
algorithm.
RTCM2 JSON FORMAT
Each RTCM2 message is dumped as a single JSON object per message, with
the message fields as attributes of that object. Arrays of satellite,
station, and constellation statistics become arrays of JSON
sub-objects. Each sentence will normally also have a "device" field
containing the pathname of the originating device.
All attributes other than the device field are mandatory. Header
attributes are emitted before others.
Header portion
Table 16. SKY object
┌───────────────┬─────────┬─────────────────────────────┐
│Name │ Type │ │
│ │ │ Description │
├───────────────┼─────────┼─────────────────────────────┤
│class │ string │ │
│ │ │ Fixed: │
│ │ │ "RTCM2". │
├───────────────┼─────────┼─────────────────────────────┤
│type │ integer │ │
│ │ │ Message │
│ │ │ type (1-9). │
├───────────────┼─────────┼─────────────────────────────┤
│station_id │ integer │ │
│ │ │ The id of │
│ │ │ the GPS │
│ │ │ reference │
│ │ │ receiver. │
│ │ │ The LF │
│ │ │ transmitters │
│ │ │ also have │
│ │ │ (different) │
│ │ │ id numbers. │
├───────────────┼─────────┼─────────────────────────────┤
│zcount │ real │ │
│ │ │ The │
│ │ │ reference │
│ │ │ time of the │
│ │ │ corrections │
│ │ │ in the │
│ │ │ message in │
│ │ │ seconds │
│ │ │ within the │
│ │ │ current │
│ │ │ hour. Note │
│ │ │ that it is │
│ │ │ in GPS time, │
│ │ │ which is │
│ │ │ some seconds │
│ │ │ ahead of UTC │
│ │ │ (see the │
│ │ │ U.S. Naval │
│ │ │ Observatory's │
│ │ │ table of │
│ │ │ leap second │
│ │ │ corrections[2]). │
├───────────────┼─────────┼─────────────────────────────┤
│seqnum │ integer │ │
│ │ │ Sequence number. │
│ │ │ Only 3 bits │
│ │ │ wide, wraps │
│ │ │ after 7. │
├───────────────┼─────────┼─────────────────────────────┤
│length │ integer │ │
│ │ │ The number of │
│ │ │ words after the │
│ │ │ header that │
│ │ │ comprise the │
│ │ │ message. │
├───────────────┼─────────┼─────────────────────────────┤
│station_health │ integer │ │
│ │ │ Station │
│ │ │ transmission │
│ │ │ status. │
│ │ │ Indicates the │
│ │ │ health of the │
│ │ │ beacon as a │
│ │ │ reference │
│ │ │ source. Any │
│ │ │ nonzero value │
│ │ │ means the │
│ │ │ satellite is │
│ │ │ probably │
│ │ │ transmitting bad │
│ │ │ data and should │
│ │ │ not be used in a │
│ │ │ fix. 6 means the │
│ │ │ transmission is │
│ │ │ unmonitored. 7 │
│ │ │ means the │
│ │ │ station is not │
│ │ │ working │
│ │ │ properly. Other │
│ │ │ values are │
│ │ │ defined by the │
│ │ │ beacon operator. │
└───────────────┴─────────┴─────────────────────────────┘
<message type> is one of
1
full corrections - one message containing corrections for all
GPS satellites in view. This is not common.
3
reference station parameters - the position of the reference
station GPS antenna.
4
datum — the datum to which the DGPS data is referred.
5
constellation health — information about the satellites the
beacon can see.
6
null message — just a filler.
7
radio beacon almanac — information about this or other beacons.
9
subset corrections — a message containing corrections for only
a subset of the GPS satellites in view.
16
special message — a text message from the beacon operator.
31
GLONASS subset corrections — a message containing corrections
for a set of the GLONASS satellites in view.
Type 1 and 9: Correction data
One or more satellite objects follow the header for type 1 or type
9 messages. Here is the format:
Table 17. Satellite object
┌──────┬─────────┬─────────────────────────┐
│Name │ Type │ │
│ │ │ Description │
├──────┼─────────┼─────────────────────────┤
│ident │ integer │ │
│ │ │ The PRN │
│ │ │ number of │
│ │ │ the │
│ │ │ satellite │
│ │ │ for which │
│ │ │ this is │
│ │ │ correction │
│ │ │ data. │
├──────┼─────────┼─────────────────────────┤
│udre │ integer │ │
│ │ │ User │
│ │ │ Differential │
│ │ │ Range Error │
│ │ │ (0-3). See │
│ │ │ the table │
│ │ │ following │
│ │ │ for values. │
├──────┼─────────┼─────────────────────────┤
│iod │ integer │ │
│ │ │ Issue Of │
│ │ │ Data, │
│ │ │ matching the │
│ │ │ IOD for the │
│ │ │ current │
│ │ │ ephemeris of │
│ │ │ this │
│ │ │ satellite, │
│ │ │ as │
│ │ │ transmitted │
│ │ │ by the │
│ │ │ satellite. │
│ │ │ The IOD is a │
│ │ │ unique tag │
│ │ │ that │
│ │ │ identifies │
│ │ │ the │
│ │ │ ephemeris; │
│ │ │ the GPS │
│ │ │ using the │
│ │ │ DGPS │
│ │ │ correction │
│ │ │ and the DGPS │
│ │ │ generating │
│ │ │ the data │
│ │ │ must use the │
│ │ │ same orbital │
│ │ │ positions │
│ │ │ for the │
│ │ │ satellite. │
├──────┼─────────┼─────────────────────────┤
│prc │ real │ │
│ │ │ The │
│ │ │ pseudorange │
│ │ │ error in │
│ │ │ meters for │
│ │ │ this │
│ │ │ satellite as │
│ │ │ measured by │
│ │ │ the beacon │
│ │ │ reference │
│ │ │ receiver at │
│ │ │ the epoch │
│ │ │ indicated by │
│ │ │ the z_count │
│ │ │ in the │
│ │ │ parent │
│ │ │ record. │
├──────┼─────────┼─────────────────────────┤
│rrc │ real │ │
│ │ │ The rate of │
│ │ │ change of │
│ │ │ pseudorange │
│ │ │ error in │
│ │ │ meters/sec │
│ │ │ for this │
│ │ │ satellite as │
│ │ │ measured by │
│ │ │ the beacon │
│ │ │ reference │
│ │ │ receiver at │
│ │ │ the epoch │
│ │ │ indicated by │
│ │ │ the z_count │
│ │ │ field in the │
│ │ │ parent │
│ │ │ record. This │
│ │ │ is used to │
│ │ │ calculate │
│ │ │ pseudorange │
│ │ │ errors at │
│ │ │ other │
│ │ │ epochs, if │
│ │ │ required by │
│ │ │ the GPS │
│ │ │ receiver. │
└──────┴─────────┴─────────────────────────┘
User Differential Range Error values are as follows:
Table 18. UDRE values
┌──┬──────────────────────┐
│0 │ 1-sigma error <= 1m │
├──┼──────────────────────┤
│1 │ 1-sigma error <= 4m │
├──┼──────────────────────┤
│2 │ 1-sigma error <= 8m │
├──┼──────────────────────┤
│3 │ 1-sigma error > 8m │
└──┴──────────────────────┘
Here's an example:
{"class":"RTCM2","type":1,
"station_id":688,"zcount":843.0,"seqnum":5,"length":19,"station_health":6,
"satellites":[
{"ident":10,"udre":0,"iod":46,"prc":-2.400,"rrc":0.000},
{"ident":13,"udre":0,"iod":94,"prc":-4.420,"rrc":0.000},
{"ident":7,"udre":0,"iod":22,"prc":-5.160,"rrc":0.002},
{"ident":2,"udre":0,"iod":34,"prc":-6.480,"rrc":0.000},
{"ident":4,"udre":0,"iod":47,"prc":-8.860,"rrc":0.000},
{"ident":8,"udre":0,"iod":76,"prc":-7.980,"rrc":0.002},
{"ident":5,"udre":0,"iod":99,"prc":-8.260,"rrc":0.002},
{"ident":23,"udre":0,"iod":81,"prc":-8.060,"rrc":0.000},
{"ident":16,"udre":0,"iod":70,"prc":-11.740,"rrc":0.000},
{"ident":30,"udre":0,"iod":4,"prc":-18.960,"rrc":-0.006},
{"ident":29,"udre":0,"iod":101,"prc":-24.960,"rrc":-0.002}
]}
Type 3: Reference Station Parameters
Here are the payload members of a type 3 (Reference Station
Parameters) message:
Table 19. Reference Station Parameters
┌─────┬──────┬────────────────────────┐
│Name │ Type │ │
│ │ │ Description │
├─────┼──────┼────────────────────────┤
│x │ real │ │
│ │ │ ECEF X │
│ │ │ coordinate. │
├─────┼──────┼────────────────────────┤
│y │ real │ │
│ │ │ ECEF Y │
│ │ │ coordinate. │
├─────┼──────┼────────────────────────┤
│z │ real │ │
│ │ │ ECEF Z │
│ │ │ coordinate. │
└─────┴──────┴────────────────────────┘
The coordinates are the position of the station, in meters to two
decimal places, in Earth Centred Earth Fixed coordinates. These are
usually referred to the WGS84 reference frame, but may be referred
to NAD83 in the US (essentially identical to WGS84 for all except
geodesists), or to some other reference frame in other parts of the
world.
An invalid reference message is represented by a type 3 header
without payload fields.
Here's an example:
{"class":"RTCM2","type":3,
"station_id":652,"zcount":1657.2,"seqnum":2,"length":4,"station_health":6,
"x":3878620.92,"y":670281.40,"z":5002093.59
}
Type 4: Datum
Here are the payload members of a type 4 (Datum) message:
Table 20. Datum
┌───────────┬─────────┬────────────────────────┐
│Name │ Type │ │
│ │ │ Description │
├───────────┼─────────┼────────────────────────┤
│dgnss_type │ string │ │
│ │ │ Either │
│ │ │ "GPS", │
│ │ │ "GLONASS", │
│ │ │ "GALILEO", │
│ │ │ or │
│ │ │ "UNKNOWN". │
├───────────┼─────────┼────────────────────────┤
│dat │ integer │ │
│ │ │ 0 or 1 and │
│ │ │ indicates │
│ │ │ the sense │
│ │ │ of the │
│ │ │ offset │
│ │ │ shift given │
│ │ │ by dx, dy, │
│ │ │ dz. dat = 0 │
│ │ │ means that │
│ │ │ the station │
│ │ │ coordinates │
│ │ │ (in the │
│ │ │ reference │
│ │ │ message) │
│ │ │ are │
│ │ │ referred to │
│ │ │ a local │
│ │ │ datum and │
│ │ │ that adding │
│ │ │ dx, dy, dz │
│ │ │ to that │
│ │ │ position │
│ │ │ will render │
│ │ │ it in GNSS │
│ │ │ coordinates │
│ │ │ (WGS84 for │
│ │ │ GPS). If │
│ │ │ dat = 1 │
│ │ │ then the │
│ │ │ ref station │
│ │ │ position is │
│ │ │ in GNSS │
│ │ │ coordinates │
│ │ │ and adding │
│ │ │ dx, dy, dz │
│ │ │ will give │
│ │ │ it referred │
│ │ │ to the │
│ │ │ local │
│ │ │ datum. │
├───────────┼─────────┼────────────────────────┤
│datum_name │ string │ │
│ │ │ A standard │
│ │ │ name for │
│ │ │ the datum. │
├───────────┼─────────┼────────────────────────┤
│dx │ real │ │
│ │ │ X offset. │
├───────────┼─────────┼────────────────────────┤
│dy │ real │ │
│ │ │ Y offset. │
├───────────┼─────────┼────────────────────────┤
│dz │ real │ │
│ │ │ Z offset. │
└───────────┴─────────┴────────────────────────┘
<dx> <dy> <dz> are offsets to convert from local datum to GNSS
datum or vice versa. These fields are optional.
An invalid datum message is represented by a type 4 header without
payload fields.
Type 5: Constellation Health
One or more of these follow the header for type 5 messages — one
for each satellite.
Here is the format:
Table 21. Constellation health
┌────────────┬─────────┬──────────────────────────┐
│Name │ Type │ │
│ │ │ Description │
├────────────┼─────────┼──────────────────────────┤
│ident │ integer │ │
│ │ │ The PRN │
│ │ │ number of │
│ │ │ the │
│ │ │ satellite. │
├────────────┼─────────┼──────────────────────────┤
│iodl │ bool │ │
│ │ │ True │
│ │ │ indicates │
│ │ │ that this │
│ │ │ information │
│ │ │ relates to │
│ │ │ the │
│ │ │ satellite │
│ │ │ information │
│ │ │ in an │
│ │ │ accompanying │
│ │ │ type 1 or │
│ │ │ type 9 │
│ │ │ message. │
├────────────┼─────────┼──────────────────────────┤
│health │ integer │ 0 indicates that the │
│ │ │ satellite is healthy. │
│ │ │ Any other value │
│ │ │ indicates a │
│ │ │ problem (coding is not │
│ │ │ known)..PP │
├────────────┼─────────┼──────────────────────────┤
│snr │ integer │ │
│ │ │ The │
│ │ │ carrier/noise │
│ │ │ ratio of the │
│ │ │ received │
│ │ │ signal in │
│ │ │ the range 25 │
│ │ │ to 55 │
│ │ │ dB(Hz). │
├────────────┼─────────┼──────────────────────────┤
│health_en │ bool │ │
│ │ │ If set to │
│ │ │ True it │
│ │ │ indicates │
│ │ │ that the │
│ │ │ satellite is │
│ │ │ healthy even │
│ │ │ if the │
│ │ │ satellite │
│ │ │ navigation │
│ │ │ data says it │
│ │ │ is unhealthy. │
├────────────┼─────────┼──────────────────────────┤
│new_data │ bool │ True indicates that the │
│ │ │ IOD for this satellite │
│ │ │ will │
│ │ │ soon be updated │
│ │ │ in type 1 or 9 │
│ │ │ messages..PP │
├────────────┼─────────┼──────────────────────────┤
│los_warning │ bool │ │
│ │ │ Line-of-sight │
│ │ │ warning. True │
│ │ │ indicates │
│ │ │ that the │
│ │ │ satellite │
│ │ │ will shortly │
│ │ │ go unhealthy. │
├────────────┼─────────┼──────────────────────────┤
│tou │ integer │ │
│ │ │ Healthy time │
│ │ │ remaining in │
│ │ │ seconds. │
└────────────┴─────────┴──────────────────────────┘
Type 6: Null
This just indicates a null message. There are no payload fields.
Unknown message
This format is used to dump message words in hexadecimal when the
message type field doesn't match any of the known ones.
Here is the format:
Table 22. Unknown Message
┌─────┬──────┬────────────────────────┐
│Name │ Type │ │
│ │ │ Description │
├─────┼──────┼────────────────────────┤
│data │ list │ │
│ │ │ A list of │
│ │ │ strings. │
└─────┴──────┴────────────────────────┘
Each string in the array is a hex literal representing 30 bits of
information, after parity checks and inversion. The high two bits
should be ignored.
Type 7: Radio Beacon Almanac
Here is the format:
Table 23. Contellation health
┌───────────┬─────────┬───────────────────────────┐
│Name │ Type │ │
│ │ │ Description │
├───────────┼─────────┼───────────────────────────┤
│lat │ real │ │
│ │ │ Latitude in │
│ │ │ degrees, of │
│ │ │ the LF │
│ │ │ transmitter │
│ │ │ antenna for │
│ │ │ the station │
│ │ │ for which │
│ │ │ this is an │
│ │ │ almanac. │
│ │ │ North is │
│ │ │ positive. │
├───────────┼─────────┼───────────────────────────┤
│lon │ real │ │
│ │ │ Longitude │
│ │ │ in degrees, │
│ │ │ of the LF │
│ │ │ transmitter │
│ │ │ antenna for │
│ │ │ the station │
│ │ │ for which │
│ │ │ this is an │
│ │ │ almanac. │
│ │ │ East is │
│ │ │ positive. │
├───────────┼─────────┼───────────────────────────┤
│range │ integer │ Published range of the │
│ │ │ station in km..PP │
├───────────┼─────────┼───────────────────────────┤
│frequency │ real │ │
│ │ │ Station │
│ │ │ broadcast │
│ │ │ frequency │
│ │ │ in kHz. │
├───────────┼─────────┼───────────────────────────┤
│health │ integer │ │
│ │ │ <health> is │
│ │ │ the health │
│ │ │ of the │
│ │ │ station for │
│ │ │ which this │
│ │ │ is an │
│ │ │ almanac. If │
│ │ │ it is │
│ │ │ non-zero, │
│ │ │ the station │
│ │ │ is issuing │
│ │ │ suspect │
│ │ │ data and │
│ │ │ should not │
│ │ │ be used for │
│ │ │ fixes. The │
│ │ │ ITU and │
│ │ │ RTCM104 │
│ │ │ standards │
│ │ │ differ │
│ │ │ about the │
│ │ │ mode │
│ │ │ detailed │
│ │ │ interpretation │
│ │ │ of the │
│ │ │ <health> │
│ │ │ field and │
│ │ │ even about │
│ │ │ its bit │
│ │ │ width. │
├───────────┼─────────┼───────────────────────────┤
│station_id │ integer │ │
│ │ │ The id of the │
│ │ │ transmitter. │
│ │ │ This is not │
│ │ │ the same as │
│ │ │ the reference │
│ │ │ id in the │
│ │ │ header, the │
│ │ │ latter being │
│ │ │ the id of the │
│ │ │ reference │
│ │ │ receiver. │
├───────────┼─────────┼───────────────────────────┤
│bitrate │ integer │ │
│ │ │ The │
│ │ │ transmitted │
│ │ │ bitrate. │
└───────────┴─────────┴───────────────────────────┘
Here's an example:
{"class":"RTCM2","type":9,"station_id":268,"zcount":252.6,
"seqnum":4,"length":5,"station_health":0,
"satellites":[
{"ident":13,"udre":0,"iod":3,"prc":-25.940,"rrc":0.066},
{"ident":2,"udre":0,"iod":73,"prc":0.920,"rrc":-0.080},
{"ident":8,"udre":0,"iod":22,"prc":23.820,"rrc":0.014}
]}
Type 13: GPS Time of Week
Here are the payload members of a type 13 (Groumf Tramitter
Parameters) message:
Table 24. Grund Transmitter Parameters
┌──────────┬─────────┬─────────────────────────┐
│Name │ Type │ │
│ │ │ Description │
├──────────┼─────────┼─────────────────────────┤
│status │ bool │ │
│ │ │ If True, │
│ │ │ signals │
│ │ │ user to │
│ │ │ expect a │
│ │ │ type 16 │
│ │ │ explanatory │
│ │ │ message │
│ │ │ associated │
│ │ │ with this │
│ │ │ station. │
│ │ │ Probably │
│ │ │ indicates │
│ │ │ some sort │
│ │ │ of unusual │
│ │ │ event. │
├──────────┼─────────┼─────────────────────────┤
│rangeflag │ bool │ │
│ │ │ If True, │
│ │ │ indicates │
│ │ │ that the │
│ │ │ estimated │
│ │ │ range is │
│ │ │ different │
│ │ │ from that │
│ │ │ found in │
│ │ │ the Type 7 │
│ │ │ message │
│ │ │ (which │
│ │ │ contains │
│ │ │ the │
│ │ │ beacon's │
│ │ │ listed │
│ │ │ range). │
│ │ │ Generally │
│ │ │ indicates a │
│ │ │ range │
│ │ │ reduction │
│ │ │ due to │
│ │ │ causes such │
│ │ │ as poor │
│ │ │ ionospheric │
│ │ │ conditions │
│ │ │ or reduced │
│ │ │ transmission │
│ │ │ power. │
├──────────┼─────────┼─────────────────────────┤
│lat │ real │ │
│ │ │ Degrees │
│ │ │ latitude, │
│ │ │ signed. │
│ │ │ Positive is │
│ │ │ N, negative │
│ │ │ is S. │
├──────────┼─────────┼─────────────────────────┤
│lon │ real │ │
│ │ │ Degrees │
│ │ │ longitude, │
│ │ │ signed. │
│ │ │ Positive is │
│ │ │ E, negative │
│ │ │ is W. │
├──────────┼─────────┼─────────────────────────┤
│range │ integer │ │
│ │ │ Transmission │
│ │ │ range in km │
│ │ │ (1-1024). │
└──────────┴─────────┴─────────────────────────┘
This message type replaces message type 3 (Reference Station
Parameters) in RTCM 2.3.
Type 14: GPS Time of Week
Here are the payload members of a type 14 (GPS Time of Week)
message:
Table 25. Reference Station Parameters
┌─────────┬─────────┬────────────────────────┐
│Name │ Type │ │
│ │ │ Description │
├─────────┼─────────┼────────────────────────┤
│week │ integer │ │
│ │ │ GPS week │
│ │ │ (0-123). │
├─────────┼─────────┼────────────────────────┤
│hour │ integer │ │
│ │ │ Hour of │
│ │ │ week │
│ │ │ (0-167). │
├─────────┼─────────┼────────────────────────┤
│leapsecs │ integer │ │
│ │ │ Leap │
│ │ │ Seconds │
│ │ │ (0-63). │
└─────────┴─────────┴────────────────────────┘
Here's an example:
{"class":"RTCM2","type":14,"station_id":652,"zcount":1657.2,
"seqnum":3,"length":1,"station_health":6,"week":601,"hour":109,
"leapsecs":15}
Type 16: Special Message
Table 26. Special Message
┌────────┬────────┬────────────────────────┐
│Name │ Type │ │
│ │ │ Description │
├────────┼────────┼────────────────────────┤
│message │ string │ │
│ │ │ A text │
│ │ │ message │
│ │ │ sent by the │
│ │ │ beacon │
│ │ │ operator. │
└────────┴────────┴────────────────────────┘
Type 31: Correction data
One or more GLONASS satellite objects follow the header for type 1
or type 9 messages. Here is the format:
Table 27. Satellite object
┌───────┬──────────┬────────────────────────────────┐
│Name │ Type │ │
│ │ │ Description │
├───────┼──────────┼────────────────────────────────┤
│ident │ integer │ │
│ │ │ The PRN │
│ │ │ number of │
│ │ │ the │
│ │ │ satellite │
│ │ │ for which │
│ │ │ this is │
│ │ │ correction │
│ │ │ data. │
├───────┼──────────┼────────────────────────────────┤
│udre │ integer │ │
│ │ │ User │
│ │ │ Differential │
│ │ │ Range Error │
│ │ │ (0-3). See │
│ │ │ the table │
│ │ │ following │
│ │ │ for values. │
├───────┼──────────┼────────────────────────────────┤
│change │ boolean │ │
│ │ │ Change-of-ephemeris │
│ │ │ bit. │
├───────┼──────────┼────────────────────────────────┤
│tod │ uinteger │ │
│ │ │ Count of 30-second │
│ │ │ periods since the │
│ │ │ top of the hour. │
├───────┼──────────┼────────────────────────────────┤
│prc │ real │ │
│ │ │ The pseudorange │
│ │ │ error in meters for │
│ │ │ this satellite as │
│ │ │ measured by the │
│ │ │ beacon reference │
│ │ │ receiver at the │
│ │ │ epoch indicated by │
│ │ │ the z_count in the │
│ │ │ parent record. │
├───────┼──────────┼────────────────────────────────┤
│rrc │ real │ │
│ │ │ The rate of change │
│ │ │ of pseudorange │
│ │ │ error in meters/sec │
│ │ │ for this satellite │
│ │ │ as measured by the │
│ │ │ beacon reference │
│ │ │ receiver at the │
│ │ │ epoch indicated by │
│ │ │ the z_count field │
│ │ │ in the parent │
│ │ │ record. This is │
│ │ │ used to calculate │
│ │ │ pseudorange errors │
│ │ │ at other epochs, if │
│ │ │ required by the GPS │
│ │ │ receiver. │
└───────┴──────────┴────────────────────────────────┘
Here's an example:
{"class":"RTCM2","type":31,"station_id":652,"zcount":1642.2,
"seqnum":0,"length":14,"station_health":6,
"satellites":[
{"ident":5,"udre":0,"change":false,"tod":0,"prc":132.360,"rrc":0.000},
{"ident":15,"udre":0,"change":false,"tod":0,"prc":134.840,"rrc":0.002},
{"ident":14,"udre":0,"change":false,"tod":0,"prc":141.520,"rrc":0.000},
{"ident":6,"udre":0,"change":false,"tod":0,"prc":127.000,"rrc":0.000},
{"ident":21,"udre":0,"change":false,"tod":0,"prc":128.780,"rrc":0.000},
{"ident":22,"udre":0,"change":false,"tod":0,"prc":125.260,"rrc":0.002},
{"ident":20,"udre":0,"change":false,"tod":0,"prc":117.280,"rrc":-0.004},
{"ident":16,"udre":0,"change":false,"tod":17,"prc":113.460,"rrc":0.018}
]}
RTCM3 DUMP FORMAT
The support for RTCM104v3 dumping is incomplete and buggy. Do not
attempt to use it for production! Anyone interested in it should read
the source code.
AIS DUMP FORMATS
AIS support is an extension. It may not be present if your instance of
gpsd has been built with a restricted feature set.
AIS packets are dumped as JSON objects with class "AIS". Each AIS
report object contains a "type" field giving the AIS message type and a
"scaled" field telling whether the remainder of the fields are dumped
in scaled or unscaled form. (These will be emitted before any
type-specific fields.) It will also contain a "device" field naming the
data source. Other fields have names and types as specified in the
AIVDM/AIVDO Protocol Decoding document on the GPSD project website;
each message field table may be directly interpreted as a specification
for the members of the corresponding JSON object type.
By default, certain scaling and conversion operations are performed for
JSON output. Latitudes and longitudes are scaled to decimal degrees
rather than the native AIS unit of 1/10000th of a minute of arc. Ship
(but not air) speeds are scaled to knots rather than tenth-of-knot
units. Rate of turn may appear as "nan" if is unavailable, or as one of
the strings "fastright" or "fastleft" if it is out of the AIS encoding
range; otherwise it is quadratically mapped back to the turn sensor
number in degrees per minute. Vessel draughts are converted to decimal
meters rather than native AIS decimeters. Various other scaling
conversions are described in "AIVDM/AIVDO Protocol Decoding".
SUBFRAME DUMP FORMATS
Subframe support is always compiled into gpsd but many GPSes do not
output subframe data or the gpsd driver may not support subframes.
Subframe packets are dumped as JSON objects with class "SUBFRAME". Each
subframe report object contains a "frame" field giving the subframe
number, a "tSV" field for the transmitting satellite number, a "TOW17"
field containing the 17 MSBs of the start of the next 12-second message
and a "scaled" field telling whether the remainder of the fields are
dumped in scaled or unscaled form. It will also contain a "device"
field naming the data source. Each SUBFRAME object will have a
sub-object specific to that subframe page type. Those sub-object fields
have names and types similar to those specified in the IS-GPS-200E
document; each message field table may be directly interpreted as a
specification for the members of the corresponding JSON object type.
SEE ALSOgpsd(8), libgps(3),
AUTHOR
The protocol was designed and documented by Eric S. Raymond.
NOTES
1. Radio Technical Commission for Maritime Services
http://www.rtcm.org/
2. table of leap second corrections
ftp://maia.usno.navy.mil/ser7/tai-utc.dat
The GPSD Project 28 Aug 2011 GPSD_JSON(5)