It’s been quite a while since I’ve updated my guide to the RTKLIB configuration file. Since the last update I’ve added a couple of new features and learned a bit more about some of the existing features. For previous updates, I’ve just updated the original post, but this time I thought I would re-publish it to make it easier to find.
One of the nice things about RTKLIB is that it is extremely configurable and has a whole slew of input options available. Unfortunately these can be a bit overwhelming at times, especially for someone new to the software. The RTKLIB manual does briefly explain what each option does, but even with this information it can be difficult to know how best to choose values for some of the parameters.
I won’t try to give a comprehensive explanation of all the input options here, but will explain the ones I have found useful to adjust in my experiments and include a little about why I chose the values I did. I describe them as they appear in the configuration file rather than how they appear in the RTKNAVI GUI menu but the comments apply to both. I created this list by comparing my latest config files to the default config file and noting which settings were different. The values in the list below are the values I use in my config file for a 5 Hz rover measurement rate. The same config files can be used for either RTKNAVI, RTKPOST, or RNX2RTKP.
The settings and options highlighted in blue below are available only in my demo code and not in the release code but otherwise much of what I describe below will apply to either code. Most of my work is done for RTK solutions with Ublox M8N and M8T receivers and short baselines and these settings will more directly apply to these combinations but should be useful at least as a starting point for other scenarios.
This post is intended to be used as a supplement to the RTKLIB manual, not as a standalone document, so please refer to it for information on any of the input parameters not covered here.
SETTING1:
pos1-posmode = static, kinematic, static-start, movingbase, fixed
If the rover is stationary, use “static”. If it is moving, use “kinematic” or “static-start”. “Static-start” will assume the rover is stationary until first fix is achieved and then switch to dynamic mode, allowing the kalman filter to take advantage of the knowledge that the rover is not moving initially. You can use “movingbase” if the base is moving as well as the rover, but it is not required unless the base is moving long distances. I often find that “kinematic” gives better solutions than “movingbase” even when the base is moving. “Movingbase” mode is not compatible with dynamics, so be sure not to enable both at the same time. If the base and rover remain at a fixed distance apart, set “pos2-baselen” and “pos2-basesig” when in “movingbase” mode. Use “fixed” if you know the rover’s exact location and are only interested in analyzing the residuals.
pos1-frequency = l1
“l1” for single frequency receivers, “l1+l2” if the rover is dual frequency GPS/GLONASS/Bediou, “l1+l2+e5b” if Galileo E5b is included. Starting with the dem05 b33 code, Galileo E5b is included in the L2 solution, so “l1+l2” is equivalent to “l1+l2+e5b”
pos1-soltype = forward, backward, combined
This is the direction in time that the kalman filter is run. For real-time processing, “forward” is your only choice. For post-processing, “combined” first runs the filter forward, then backwards and combines the results. For each epoch, if both directions have a fix, then the combined result is the average of the two with a fixed status unless the difference between the two is too large in which case the status will be float. If only one direction has a fix, that value will be used and the status will be fixed. If both directions are float then the average will be used and the status will be float. Results are not always better with combined because a false fix when running in either direction will usually cause the combined result to be float and incorrect. The primary advantage of combined is that it will usually give you fixed status right to the beginning of the data while the forward only solution will take some time to converge. The 2.4.3 code always resets the bias states before starting the backwards run to insure independent solutions. The demo5 code doesn’t reset the bias states to avoid having to lock back up when the rover is moving if ambiguity resolution is set to “continuous” but does reset them if it is set to “fix-and-hold”. I only use the “backward” setting for debug when I am having trouble getting an initial fix and want to know what the correct satellite phase-biases are.
pos1-elmask = 15 (degrees)
Minimum satellite elevation for use in calculating position. I usually set this to 10-15 degrees to reduce the chance of bringing multipath into the solution but this setting will be dependent on the rover environment. The more open the sky view, the lower this value can be set to.
pos1-snrmask-r = off, pos1-snrmask-b = off,on
Minimum satellite SNR for rover (_r) and base(_b) for use in calculating position. Can be a more effective criteria for eliminating poor satellites than elevation because it is a more direct measure of signal quality but the optimal value will vary with receiver type and antenna type so I leave it off most of the time to avoid the need to tune it for each application.
pos1-snrmask_L1 =35,35,35,35,35,35,35,35,35
Set SNR thresholds for each five degrees of elevation. I usually leave all values the same and pick something between 35 and 38 db depending on what the nominal SNR is. These values are only used if pos1-snrmask_x is set to on. If you are using dual frequencies, you will need to also set “pos1-snrmask_L2”
pos1-dynamics = on
Enabling rover dynamics adds velocity and acceleration states to the kalman filter for the rover. It will improve “kinematic” and “static-start” results, but will have little or no effect on “static” mode. The release code will run noticeably slower with dynamics enabled but the demo5 code should be OK. Be sure to set “prnaccelh” and “prnaccelv” appropriately for your rover acceleration characteristics. Rover dynamics is not compatible with “movingbase” mode, so turn it off when using that mode.
pos1-posopt1 = off, on (Sat PCV)
Set whether the satellite antenna phase center variation is used or not. Leave it off for RTK but you set it for PPP. If set to on, you need to specify the satellite antenna PCV file in the files parameters.
pos1-posopt2 = off, on (Rec PCV)
Set whether the receiver antenna phase center variations are used or not. If set to on, you need to specify the receiver antenna PCV file in the files parameters and the type of receiver antenna for base and rover in the antenna section. Only survey grade antennas are included in the antenna file available from IGS so only use this if your antenna is in the file. It primarily affects accuracy in the z-axis so it can be important if you care about height. You can leave this off if both antennas are the same since they will cancel.
pos1-posopt5 = off, on (RAIM FDE)
If the residuals for any satellite exceed a threshold, that satellite is excluded. This will only exclude satellites with very large errors but requires a fair bit of computation so I usually leave this disabled.
pos1-exclsats=
If you know a satellite is bad you can exclude it from the solution by listing it here. I only use this in rare cases for debugging if I suspect a satellite is bad.
pos1-navsys = 7, 15,
I always include GLONASS and SBAS sats, as more information is generally better. If using the newer 3.0 u-blox firmware with the M8T I also enable Galileo.
SETTING2:
pos2-armode = continuous, fix-and-hold
Integer ambiguity resolution method. “Continuous” mode does not take advantage of fixes to adjust the phase bias states so it is the most immune to false fixes. “Fix-and-hold” does use feedback from the fixes to help track the ambiguities. I prefer to use “fix-and-hold” and adjust the tracking gain (pos2-varholdamb) low enough to minimize the chance of a false fix. If “armode” is not set to “fix-and-hold” then any of the options below that refer to holds don’t apply, including pos2-gloarmode.
pos2-varholdamb=0.001, 0.1 (meters)
In the demo5 code, the tracking gain for fix-and-hold can be adjusted with this parameter. It is actually a variance rather than a gain, so larger values will give lower gain. 0.001 is the default value, anything over 100 will have very little effect. This value is used as the variance for the pseudo-measurements generated during a hold which provide feedback to drive the bias states in the kalman filter towards integer values. I find that values from 0.1 to 1.0 provides enough gain to assist with tracking while still avoiding tracking of false fixes in most cases.
pos2-gloarmode = on, fix-and-hold, autocal
Integer ambiguity resolution for the GLONASS sats. If your receivers are identical, you can usually set this to “on” which is the preferred setting since it will allow the GLONASS sats to be used for integer ambiguity resolution during the initial acquire. If your receivers are different or you are using two u-blox M8N receivers you will need to null out the inter-channel biases with this parameter set to “fix-and-hold” if you want to include the GLONASS satellites in the AR solution. In this case the GLONASS sats will not be used for ambiguity resolution until after the inter-channel biases have been calibrated which begins after the first hold. There is an “autocal” option as well, but I have never been able to make this work in the 2.4.3 code. In the demo5 code I have added the capability to this feature to preset the initial inter-channel bias, variance, and calibration gain. I then set the biases to known values for the particular receiver pair and set the gain very low. This defeats the auto calibration aspect of the feature but does provide a mechanism to specify the biases which is otherwise missing in RTKLIB. When “autocal” is used, the GLONASS satellites will be used for the initial acquire. The “autocal” feature can also be used to determine the inter-channel biases with a zero or short baseline using an iterative approach.
pos2-gainholdamb=0.01
In the demo5 code, the gain of the inter-channel bias calibration for the GLONASS satellites can be adjusted with this parameter.
pos2-arthres = 3
This is the threshold used to determine if there is enough confidence in the ambiguity resolution solution to declare a fix. It is the ratio of the squared residuals of the second-best solution to the best solution. I generally always leave this at the default value of 3.0 and adjust all the other parameters to work around this one. Although a larger AR ratio indicates higher confidence than a low AR ratio, there is not a fixed relationship between the two. The larger the errors in the kalman filter states, the lower the confidence in that solution will be for a given AR ratio. Generally the errors in the kalman filter will be largest when it is first converging so this is the most likely time to get a false fix. Reducing pos2-arthers1 can help avoid this.
pos2-arfilter = on
Setting this to on will qualify new sats or sats recovering from a cycle-slip. If a sat significantly degrades the AR ratio when it is first added, its use for ambiguity resolution will be delayed. Turning this on should allow you to reduce “arlockcnt” which serves a similar purpose but with a blind delay count.
pos2-arthres1 = 0.004-0.10
Integer ambiguity resolution is delayed until the variance of the position state has reached this threshold. It is intended to avoid false fixes before the bias states in the kalman filter have had time to converge. It is particularly important to set this to a relatively low value if you have set eratio1 to values larger than 100 or are using a single constellation solution. If you see AR ratios of zero extending too far into your solution, you may need to increase this value since it means ambiguity resolution has been disabled because the threshold has not been met yet. I find 0.004 to 0.10 usually works well for me but if your measurements are lower quality you may need to increase this to avoid overly delaying first fix or losing fix after multiple cycle slips have occurred.
pos2-arthres2
Relative GLONASS hardware bias in meters per frequency slot. This parameter is only used when pos2-gloarmode is set to “autocal” and is used to specify the inter-channel bias between two different receiver manufacturers. To find the appropriate values for common receiver types, as well as how to use this parameter for an iterative search to find values for receiver types not specified, see this post. This parameter is defined but unused in RTKLIB 2.4.3
pos2-arthres3 = 1e-9,1e-7
Initial variance of the GLONASS hardware bias state. This parameter is only used when pos2-gloarmode is set to “autocal”. A smaller value will give more weight to the initial value specified in pos2-arthres2. I use 1e-9 when pos2-arthres2 is set to a known bias, and 1e-7 for iterative searches. This parameter is defined but unused in RTKLIB 2.4.3
pos2-arthres4 = 0.00001,0.001
Kalman filter process noise for the GLONASS hardware bias state. A smaller value will give more weight to the initial value specified in pos2-arthres2. I use 0.00001 when pos2-arthres2 is set to a known bias, and 0.001 for iterative searches. This parameter is defined but unused in RTKLIB 2.4.3
pos2-arlockcnt = 0, 5
Number of samples to delay a new sat or sat recovering from a cycle-slip before using it for integer ambiguity resolution. Avoids corruption of the AR ratio from including a sat that hasn’t had time to converge yet. Use in conjunction with “arfilter”. Note that the units are in samples, not units of time, so it must be adjusted if you change the rover measurement sample rate. I usually set this to zero for u-blox receivers which are very good at flagging questionable observations but set it to at least five for other receivers. If not using the demo5 RTKLIB code, set this higher since the “arfilter” feature is not supported.
pos2-minfixsats = 4
Minimum number of sats necessary to get a fix. Used to avoid false fixes from a very small number of satellites, especially during periods of frequent cycle-slips.
pos2-minholdsats = 5
Minimum number of sats necessary to hold an integer ambiguity result. Used to avoid false holds from a very small number of satellites, especially during periods of frequent cycle-slips.
pos2-mindropsats = 10
Minimum number of sats necessary to enable exclusion of a single satellite from ambiguity resolution each epoch. In each epoch a different satellite is excluded. If excluding the satellite results in a significant improvement in the AR ratio, then that satellite is removed from the list of satellites used for AR.
pos2-rcvstds = on,off
Enabling this feature causes the the measurement variances for the raw pseudorange and phase measurement observations to be adjusted based on the standard deviation of the measurements as reported by the receiver. This feature is currently only supported for u-blox receivers. The adjustment in variance is in addition to adjustments made for satellite elevation based on the stats-errphaseel parameter. I generally get better results with this turned off.
pos2-arelmask = 15
Functionally no different from the default of zero, since elevations less than “elmask” will not be used for ambiguity resolution but I changed it to avoid confusion.
pos2-arminfix = 20-100 (5-20*sample rate)
Number of consecutive fix samples needed to hold the ambiguities. Increasing this is probably the most effective way to reduce false holds, but will also increase time to first hold and time to reacquire a hold. As the ambiguity tracking gain is reduced (i.e. as pos2-varholdamb is increased), and the number of observations increases, arminfix can be reduced. Note that this value should also be adjusted if the rover measurement sample rate changes.
pos2-elmaskhold = 15
Functionally no different from the default of zero, since elevations less than “elmask” will not be used for holding ambiguity resolution results but I changed it to avoid confusion.
pos2-aroutcnt = 100 (20*sample rate)
Number of consecutive missing samples that will cause the ambiguities to be reset. Again, this value needs to be adjusted if the rover measurement sample rate changes.
pos2-maxage = 100
Maximum delay between rover measurement and base measurement (age of differential) in seconds. This usually occurs because of missing measurements from a misbehaving radio link. I’ve increased it from the default because I found I was often still getting good results even when this value got fairly large, assuming the dropout occurred after first fix-and-hold.
pos2-rejionno = 1000, 0.2
Reject a measurement if its pre-fit residual is greater than this value in meters. I have found that RTKLIB does not handle outlier measurements well, so I set this large enough to effectively disable it. With non-ublox receivers which typically are not as good at flagging outliers, I sometimes have to set this back to the default of 30 or even lower to attempt to handle the outliers but this is a trade-off because it can then cause other issues, particularly with initial convergence of the kalman filter.
Outlier rejection has been improved in the demo5 code starting with version b33. In addition to better handling of the outlier measurements, the way this number is applied to code and phase measurements has changed. Previously this value was applied without adjustment to both code and phase measurements. In the newer version, this value is still applied without adjustment to the phase measurements but is multiplied by eratio for the code measurements. This allows it to be set to values appropriate for the phase measurements. I usually set it to 0.2 which is very helpful to catch and reject unflagged cycle slips.
OUTPUT:
out-solformat = enu, llh, xyz
I am usually interested in relative distances between rover and base, so set this to “enu”. If you are interested in absolute locations, set this to “llh” but make sure you set the exact base location in the “ant2” settings. Be careful with this setting if you need accurate z-axis measurements. Only the llh format will give you a constant z-height if the rover is at constant altitude. “Enu” and “xyz” are cartesian coordinates and so the z-axis follows a flat plane, not the curvature of the earth. This can lead to particularly large errors if the base station is located farther from the rover since the curvature will increase with distance.
out-outhead = on
No functional difference to the solution, just output more info to the result file.
out-outopt = on
No functional difference to the solution, just output more info to the result file.
out-outstat = residual
No functional difference to the solution, just output residuals to a file. The residuals can be very useful for debugging problems with a solution and can be plotted with RTKPLOT as long as the residual file is in the same folder as the solution file.
stats-eratio1 = 300
stats-eratio2 = 300
Ratio of the standard deviations of the pseudorange measurements to the carrier-phase measurements. I have found a larger value works better for low-cost receivers, but that the default value of 100 often work better for more expensive receivers since they have less noisy pseudorange measurements. Larger values tend to cause the kalman filter to converge faster and leads to faster first fixes but it also increases the chance of a false fix. If you increase this value, you should set pos2-arthres1 low enough to prevent finding fixes before the kalman filter has had time to converge. I believe increasing this value has a similar effect to increasing the time constant on a pseudorange smoothing algorithm in that it filters out more of the higher frequencies in the pseudorange measurements while maintaining the low frequency components.
stats-prnaccelh = 3.0
If receiver dynamics are enabled, use this value to set the standard deviation of the rover receiver acceleration in the horizontal components. This value should include accelerations at all frequencies, not just low frequencies. It should characterize any movements of the rover antenna, not just movements of the complete rover so it may be larger than you think. It will include accelerations from vibration, bumps in the road, etc as well as the more obvious rigid-body accelerations of the whole rover. It can be estimated by running a solution with this value set to a large value, then examining the accel values in the solution file with RTKPLOT
stats-prnaccelv = 1.0
The comments about horizontal accelerations apply even more to the vertical acceleration component since in many applications the intentional accelerations will all be in the horizontal components. It is best to derive this value from actual GPS measurement data rather than expectations of the rigid-body rover. It is better to over-estimate these values than to under-estimate them.
ant2-postype = rinexhead, llh, single
This is the location of the base station antenna. If you are only interested in relative distance between base and rover this value does not need to be particularly accurate. For post-processing I usually use the approximate base station location from the RINEX file header. If you want absolute position in your solution, then the base station location must be much more accurate since any error in that will add to your rover position error. If I want absolute position, I first process the base station data against a nearby reference station to get the exact location, then use the ”llh” or “xyz”option to specify that location. For real-time processing, I use the “single” option which uses the single solution from the data to get a rough estimate of base station location.
ant2-maxaveep = 1
Specifies the number of samples averaged to determine base station location if “postype” is set to “single”. I set this to one to prevent the base station position from varying after the kalman filter has started to converge since that seems to cause long times to first fix. In most cases for post-processing, the base station location will come from the RINEX file header and so you will not use this setting. However if you are working with RTCM files you may need this even for post-processing.
MISC:
misc-timeinterp =off,on
Interpolates the base station observations. I generally set this to “on” if the base station observations sample time is larger than 5 seconds.
Please help me update this list if you have had success adjusting other options or using different settings for these options, or if you disagree with any of my suggestions. I will treat this as a working document and continue to update it as I learn more.
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