The following product styles are shipped with ODTK:
Product Styles  

Style  Description 
Accelerometer Bias  Displays Accelerometer Sensor Bias error estimates and 2sigma error bounds, derived from the state covariance. The units on the graphs and reports are fixed and are nanometers/sec^{2}. 
Accelerometer BiasDrift  Displays Accelerometer Sensor Bias Drift error estimates and 2sigma error bounds, derived from the state covariance. The units on the graphs and reports are fixed and are nanometers/sec^{3}. 
Accelerometer ScaleFactor  Displays Accelerometer Scale Factor error estimates and 2sigma error bounds, derived from the state covariance. 
Accelerometer Measurement Listing  Displays the Accelerometer linear acceleration measurements in millimeters/sec^{2}. Note that the size of linear acceleration measurement in its nominal units (m/sec^{2}) precludes the use of other predefined measurement listing styles. 
Allan Variance  Computes and displays clock Allan Variance data from the clock phase estimates. The Allan Variance data is meant to be displayed on a loglog plot. To create a loglog plot, use the graph customization to change the X, Y axes to log, log (under the AXIS tab) and to turn on the grid lines (under the GENERAL tab). 
Antenna Loc Consistency  Displays Consistency Test statistics for antenna location on spacecraft body state differences (difrun) between two processes. A process can be a simulator, a filter or a smoother. Valid for differences generated by State Difference Tool, found on the LaunchPad Utilities tab. 
Antenna Location  Displays Antenna X, Y, and Z Location Estimate in Body Frame. Valid for filter and smoother. 
Antenna Location X, Y, Z  Displays Antenna X, Y, or Z Location Estimate in Body Frame together with +/ 2sigma bounds from covariance. Valid for filter and smoother. 
Atmosphere Density Consistency  Graphs the FilterSmoother Consistency Test value and statistic for the atmospheric density correction state parameter. Valid for differences generated by the State Difference Tool, found on the LaunchPad Utilities tab. 
Atmosphere Density Estimate  Displays atmospheric density state estimate (Dr/r) and 0.95P bounds, derived from the state covariance. Valid for simulator, filter or smoother. 
Atmosphere Density Total  Displays the model value for atmospheric density (e.g. from the CIRA 1972 model) and (model value + estimated correction), versus time. Valid for simulator, filter or smoother. 
Avg Sat Force Model Biases  Tabulates for each force model bias parameter in state space (i.e. atmospheric density, ballistic coefficient and solar pressure) the mean estimated bias together with the median, maximum and minimum bias estimates. The mean is the average of the bias estimates following the measurement update correction considering (only) measurements associated the given satellite. Valid for filter only. 
Avg Tracker Biases  Tabulates for each measurement bias parameter in state space the mean estimated bias together with the median, maximum and minimum bias estimates. The mean is the average of the bias estimates following the measurement update correction considering (only) measurements involving the associated tracker bias measurement type. Valid for filter only. 
Avg Transponder Biases  Tabulates for each transponder bias parameter in state space the mean estimated bias together with the median, maximum and minimum bias estimates. The mean is the average of the bias estimates following the measurement update correction considering (only) measurements involving the associated transponder. Valid for filter only. When processing multiple measurement types, the filter's Output.DataArchive.SaveOnlyLastMeasPerStep may need to be set to false for this report to resolve transponders with associated measurement updates. 
Ballistic Coefficient  This graph style provides graphs of the ballistic coefficient state parameter, as the estimate (DB/B) and the corresponding error root variance. The Ballistic Coefficient report style tabulates these quantities and computes a corrected B value. 
Ballistic Coefficient Consistency  Graphs the FilterSmoother Consistency Test value and statistic for ballistic coefficient state parameter. Valid for differences generated by State Difference Tool, found on the LaunchPad Utilities tab. 
Clock Aging  Displays GPS satellite or GPS receiver estimates and 2sigma values for clock aging, the second derivative of clock phase. The units on the graphs and reports are chosen to agree with the units in the Object Properties window. 
Clock Consistency  Provides Consistency Test statistics for clock phase and clock drift for state differences (difrun) between two runfiles, nominally a filrun and a smtrun file. If the filter and smoother covariances are realistic then this test statistic is nominally between + or  3 in every state of state space. 
Clock Freq  Displays GPS satellite or GPS receiver clock frequency error estimates and 2sigma error bounds, derived from the state covariance. The units on the graphs and reports are chosen to agree with the units in the Object Properties window. 
Clock Phase  Displays GPS satellite or GPS receiver clock phase error estimate and 2sigma error bounds, derived from the state covariance. The units on the graphs and reports are chosen to agree with the units in the Object Properties window. 
Compact Meas Report  This report provides an economical version of the Measurements report. A single line contains all of the measurements collected by a facility or tracker at the same time. Color coding is used to distinguish measurement types and a grey background is provided to identify the start of a new tracking pass. 
Compact Meas Sig Report  This report is an extension to the Compact Meas report, providing measurement sigmas if they are included with the tracking data. 
Compact Residual Report  This report provides an economical version of the Measurement Residuals report. A single line contains all of the residuals, residual ratios and rejection flags computed for a facility or tracker at the same time. Color coding is used to distinguish measurement types, and a grey background is provided to identify the start of a new tracking pass. 
Cross Correlation  Displays the cross correlations between two state parameters. Select parameters of interest from Static Bowser / Inputs / data limiting. Valid for filter or smoother. 
Daily Avg Sat Force Model Biases  Tabulates for each force model bias parameter in state space (i.e. atmospheric density, ballistic coefficient and solar pressure) the mean estimated bias together with the median, maximum and minimum bias estimates. The mean is the average of the bias estimates following the measurement update correction considering (only) measurements associated the given satellite. Data is averaged across one day at a time. Valid for filter only. 
Daily Avg Tracker Biases  Tabulates for each measurement bias parameter in state space the mean estimated bias together with the median, maximum and minimum bias estimates. The mean is the average of the bias estimates following the measurement update correction considering (only) measurements involving the associated tracker bias measurement type. Data is averaged across one day at a time. Valid for filter only. 
Daily Avg Transponder Biases  Tabulates for each transponder bias parameter in state space the mean estimated bias together with the median, maximum and minimum bias estimates. The mean is the average of the bias estimates following the measurement update correction considering (only) measurements involving the associated transponder. Data is averaged across one day at a time. Valid for filter only. When processing multiple measurement types, the filter's Output.DataArchive.SaveOnlyLastMeasPerStep may need to be set to false for this report to resolve transponders with associated measurement updates. 
Data File Summary  The Data File Summary report—which is valid for a simulator, filter or smoother run file—provides file summary and file content information for three of the input files containing environmental data: the flux (space weather) file, the EOP file, and the JPL planetary ephemeris file. For each file, the data span is reported, and for the first two file types, the file modification time is reported as well. 
Differenced Antenna Location  Displays antenna location on spacecraft body state differences (difrun) between two processes. A process can be a simulator, a filter or a smoother. Valid for differences generated by State Difference Tool, found on the LaunchPad Utilities tab. 
Differenced Atmos Density  Displays the difference between the atmospheric density state estimates (Dr/r) from two processes, and displays the corresponding 0.95P bounds from both processes. A process can be a simulator, a filter or a smoother. Valid for differences generated by State Difference Tool, found on the LaunchPad Utilities tab. 
Differenced Ballistic Coefficient  Displays the difference between the ballistic coefficient state estimates (DB/B) from two processes, and displays the corresponding 0.95P bounds from both processes. A process can be a simulator, a filter or a smoother. Valid for differences generated by the State Difference Tool, found on the LaunchPad Utilities tab. 
Differenced Classical Element "x", where "x" is (a, e, i, u, O,
w) and a = semimajor axis e = eccentricity i = inclination u = true argument of latitude O = node w = argument of perigee 
Graph styles which displays the difference between the given classical element estimates from two processes, and displays the corresponding 0.95P bounds from both processes. A process can be a simulator, a filter or a smoother. Valid for differences generated by State Difference Tool, found on the LaunchPad Utilities tab. NOTE: The differenced classical elements are computed by first transforming the Cartesian elements of the two processes to the classical element set, and then subtracting the two classical element sets. In doing the transformation, the Earth Gravitational Constant (μ) associated with the gravity field of the Reference process is used in the transformation for both the Reference and Target Processes (regardless of the value of μ for the Target Process). 
Differenced Classical Elements 
Report style that displays the difference between the given classical element estimates from two processes where a process can be a simulator, a filter or a smoother. Valid for differences generated by State Difference Tool, found on the LaunchPad Utilities tab. Note that error bounds are not reported. See note in "Differenced Classical Element" style. 
Differenced Clock Aging  Displays the difference between the GPS satellite or GPS receiver clock aging error estimates from two processes, and displays the corresponding 0.95P bounds from both processes. A process can be a simulator, a filter or a smoother. Valid for differences generated by the StateDiffTool, one of the Utilities found on LaunchPad. 
Differenced Clock Freq  Displays the difference between the GPS receiver or GPS satellite clock frequency error estimates from two processes, and displays the corresponding 0.95P bounds from both processes. A process can be a simulator, a filter or a smoother. Valid for differences generated by State Difference Tool, found on the LaunchPad Utilities tab. 
Differenced Clock Phase  Displays the difference between the GPS receiver or GPS satellite clock phase error estimates from two processes, and displays the corresponding 0.95P bounds from both processes. A process can be a simulator, a filter or a smoother. Valid for differences generated by State Difference Tool, found on the LaunchPad Utilities tab 
Differenced Drag Plugin States  Supports Drag Plugin Models. Displays, for all parameters in the model, the difference between the drag model parameter estimates from two processes, and displays the corresponding 0.95P bounds from both processes. A process can be a simulator, a filter or a smoother. Valid for differences generated by State Difference Tool, found on the LaunchPad Utilities tab. 
Differenced Fac Loc Topo  This graph style displays the facility position correction estimate differences from two processes in the topocentric local tangent frame (east, south, altitude) together with the corresponding 0.95P bounds from both processes. A process can be a simulator, a filter or a smoother. Valid for differences generated by the State Difference Tool, found on the LaunchPad Utilities tab. 
Differenced Facility Location  Tabulates facility position correction estimate differences from two processes. The position estimate differences are displayed in (x, y, z), in (east, south, altitude), and in (latitude, longitude, altitude). A process can be a simulator, a filter or a smoother. Valid for differences generated by the State Difference Tool, found on the LaunchPad Utilities tab. 
Differenced Facility Tropo  Displays tropospheric bias state differences (difrun) between two processes. A process can be a simulator, a filter or a smoother. Valid for differences generated by State Difference Tool, found on the LaunchPad Utilities tab. 
Differenced Finite Maneuver History 
Presents the differences in finite maneuver state estimates between two runfiles, in various frames. Data is provided over the duration of the maneuver. Note: For Permanent Maneuver States, the filter continually estimates these parameters, and therefore the report will span the entire runfile duration. 
Differenced Meas Bias  Displays the difference between the measurement bias estimates from two processes, and displays the corresponding 0.95P bounds from both processes. A process can be a simulator, a filter or a smoother. Valid for differences generated by State Difference Tool, found on the LaunchPad Utilities tab. 
Differenced Orbit & Clock in URE 
Differences between two GPS satellite and clock solutions are graphed in terms of the User Range Error, which is a combination of position difference and clock phase differences between two runfiles. The equation used for URE is found in AFSPC document "Standard GPS Performance Metrics," and is called "Global_ERD", which is normally used for the difference between a predicted satellite/clock state and the current OCS satellite/clock state. We simply replace "predicted" with the Target runfile and "OCS" with the Reference runfile.

Differenced Pos C  Displays the difference between the crosstrack position estimates from two processes, and displays the corresponding 0.95P bounds from both processes. A process can be a simulator, a filter or a smoother. Valid for differences generated by State Difference Tool, found on the LaunchPad Utilities tab. 
Differenced Pos I  Displays the difference between the intrack position estimates from two processes, and displays the corresponding 0.95P bounds from both processes. A process can be a simulator, a filter or a smoother. Valid for differences generated by State Difference Tool, found on the LaunchPad Utilities tab. 
Differenced Pos R  Tabulates the difference between the radial position estimates from two processes, and displays the corresponding 0.95P bounds from both processes. A process can be a simulator, a filter or a smoother. Valid for differences generated by State Difference Tool, found on the LaunchPad Utilities tab. 
Differenced RIC  Tabulates position and velocity differences. If there are multiple entries at the same time, all entries are given. Valid for differences generated by State Difference Tool, found on the LaunchPad Utilities tab. 
Differenced RIC & Sigmas  Displays position and velocity sigmas for each of two processes, and displays the corresponding state differences in RIC coordinates. A process can be a simulator, a filter or a smoother. Valid for differences generated by State Difference Tool, found on the LaunchPad Utilities tab. 
Differenced SRP Coeff  Displays the difference between the solar radiation coefficient estimates from two processes, and displays the corresponding 0.95P bounds from both processes. A process can be a simulator, a filter or a smoother. Valid for differences generated by State Difference Tool, found on the LaunchPad Utilities tab. 
Differenced SRP States  Supports Solar Pressure Reflectance Plugin Model. Displays, for all parameters in the model, the difference between the solar radiation parameter estimates from two processes, and displays the corresponding 0.95P bounds from both processes. A process can be a simulator, a filter or a smoother. Valid for differences generated by State Difference Tool, found on the LaunchPad Utilities tab. 
Differenced Trans Bias  Displays the difference between the transponder bias estimates from two processes, and displays the corresponding 0.95P bounds from both processes. A process can be a simulator, a filter or a smoother. Valid for differences generated by State Difference Tool, found on the LaunchPad Utilities tab. 
Differenced Vel C  Displays the difference between the crosstrack velocity estimates from two processes, and displays the corresponding 0.95P bounds from both processes. A process can be a simulator, a filter or a smoother. Valid for differences generated by State Difference Tool, found on the LaunchPad Utilities tab. 
Differenced Vel I  Displays the difference between the intrack velocity estimates from two processes, and displays the corresponding 0.95P bounds from both processes. A process can be a simulator, a filter or a smoother. Valid for differences generated by State Difference Tool, found on the LaunchPad Utilities tab 
Differenced Vel R  Displays the difference between the radial velocity estimates from two processes, and displays the corresponding 0.95P bounds from both processes. A process can be a simulator, a filter or a smoother. Valid for differences generated by State Difference Tool, found on the LaunchPad Utilities tab. 
Drag Plugin States  Supports Drag Plugin Models. Displays drag model parameter estimate and 0.95P bounds, derived from the state covariance for all parameters in the model. Valid for filter, smoother, and simulator. If simulator the estimate reflects the "perturbation". 
Elevation vs Azimuth  Displays the observing elevation versus observing azimuth for measurements that are Accepted, Rejected, or skipped due to Low Elevation violations. This type of graph can be useful in detecting persistent multipath phenomenology so a local horizon mask can exclude persistently bad data. 
Facility Altitude Est  This graph style displays the facility altitude correction estimate and 0.95P error bounds, derived from the state covariance. Only valid when the Facility.Estimate = Lat Lon Alt. Valid for simulator, filter and smoother. For the simulator the 0.95P error bounds are set to zero. 
Facility East Est  This graph style displays the facility position correction estimate in the east direction and 0.95P error bounds, derived from the state covariance. Valid when the Facility.Estimate = Lat Lon Alt or Facility.Estimate = Lat Lon. Valid for simulator, filter or smoother. For the simulator the 0.95P error bounds are set to zero. 
Facility Location  Tabulates facility position correction estimates and corresponding error rootvariance. The position correction estimates and error rootvariances are displayed in (x, y, z), in (east, south, altitude), and in (latitude, longitude, altitude) . Valid for simulator, filter and smoother. For the simulator the error rootvariances are set to zero. 
Facility Location Cartesian  Graphs the estimated corrections to the facility location using south, east, and altitude distances. 
Facility Location LLA  Graphs the estimated corrections to the facility location using Lat, Lon, and Altitude. 
Facility South Est  This graph style displays the facility position correction estimate in the south direction and 0.95P error bounds, derived from the state covariance. Valid when the Facility.Estimate = Lat Lon Alt or Facility.Estimate = Lat Lon. Valid for simulator, filter and smoother. For the simulator the 0.95P error bounds are set to zero. 
Finite Maneuver Consistency  Provides consistency test statistics for each inertial component of one or more finite maneuvers. 
Finite Maneuver History  Tabulates maneuver components at each time step for the duration of the maneuver. Data includes ECI, Gaussian and Frenet maneuver estimates (filter and smoother) or deviates (for simulator) and mass depletion. Valid for simulator, filter and smoother. 
Finite Maneuver States  This report is the same as the Finite Maneuver History report, except that it provides the maneuver estimates over the entire duration of the filter run, whereas the Finite Maneuver History report is limited to the duration of the maneuver. 
Finite Maneuver Summary  Tabulates the parameters of a simulated /estimated finite maneuver, including the nominal maneuver and perturbations from nominal in each of several coordinates. Valid for simulator, filter and smoother. 
Finite Mnvr Inertial Thrust States  Thrust corrections in inertial components are provided in Newtons, using instantaneous mass estimate. These units correspond to the units found in the GUI. 
Finite Mnvr RIC Thrust States  Thrust corrections in RIC components are provided in Newtons, using instantaneous mass estimate. These units correspond to the units found in the GUI. 
Finite Mnvr Thrust Magnitude and Direction  Thrust magnitude correction is provided in Newtons, using instantaneous mass estimate, while thrust direction correction is provided in degrees. These units correspond to the units found in the GUI. 
Finite Mnvr Thrust Magnitude Pct (and Direction)  Thrust magnitude correction as percentage of total thrust is provided, using instantaneous mass estimate, while thrust direction correction is provided in degrees. These units correspond to the units found in the GUI. Note there are 2 graph styles. One contains the direction estimate and one does not. 
GPS SV Data  Displays GPS SV data used in the measurement modeling of the GPS pseudorange measurements. This includes the SV position at time of signal transmission, SV clock phase bias estimate, the SV relativistic clock effect, and the SV ephemeris/clock error (1 sigma) contribution to the total measurement error variance. Valid for the filter. 
Grouped Satellite Position Velocity  Tabulates the position and velocity estimates for multiple files, grouped by time and scenario. This display has utility in comparing multiple ephemeris files on the same object, determined with different OD controls. Valid for filter and smoother. 
Histogram  Displays histogram of residual ratio (predicted residual / predicted sigma). Histograms are enabled and controlled in the filter object browser. Valid for the filter. 
Histogram Descriptive  Provides the correlations among satellites, trackers and sample size. An annotation specifying Satellite(s), Measurement Type(s), and Tracker(s), appears above each histogram. Right click in the graph and select Show Annotations to toggle between showing and hiding annotations. Hover the cursor over the histogram to activate a tool tip that specifies Satellite(s), Measurement Type(s), Tracker(s) and the DataPoint value at the cursor position. 
Histogram Summary  This graph summarizes all measurement residuals into a single histogram, according to userselected data limiting. 
Instant Maneuver Summary  Displays instantaneous maneuver in several ways. Displays nominal maneuver and deviates in various coordinate systems. Valid for simulator, filter, and smoother. 
Ionosphere Measurement Corrections  Displays ionosphere refraction corrections to the modeled measurement and the uncertainty (1 sigma) assigned to the correction. Valid for the filter. 
Least Squares Measurement Biases  Reports LS Measurement Bias solution estimates for each iteration of each stage. 
Least Squares Residuals  Tabulates all least squares residuals for all stages and all iterations. Residuals are organized by type and tracker within each iteration. Valid for least squares. Data limiting capabilities of the static product builder can be used to limit the data to residuals from a particular iteration (typically the first or last one), satellite, tracker, or measurement type. 
Least Squares Residuals GPS  Supplements the Least Squares Residuals report with a tracking strand that exposes the PRN(s) being tracked. 
Least Squares Residuals TDRSS  Supplements the Least Squares Residuals with the tracking strand for all facilities and satellites participating in the multiplelegged measurement system. 
Least Squares States  Lists each state parameter and its estimate during each iteration. Can be used to view measurement biases as well as force model and orbit parameters. 
Least Squares Summary  Tabulates summary statistics for each stage and each iteration. Within each iteration, statistics are provided for each measurement type. Valid for least squares. 
Measurement Finite(First and Second) Differences  Displays the first and second differences of the actual measurements. 
Measurement Listing  Lists all measurements from all enabled files in the Scenario.Measurements.Files list. Included with each measurement is the name of the associated measurement file. 
Measurement Pass Times  Tabulates for each measurement pass the associated satellite, tracker, start and stop times, and the number of measurements in the pass. 
Measurement Residuals  Displays measurement, residual, predicted sigma, ratio of residual to sigma, and the reason for rejecting the measurement, if any. Display is chronological. Valid for the filter. 
Measurements Residuals By Strand  Same as the Measurements Residuals report except that the grouping is by the complete tracking strand instead of just the (satellite, tracker). Useful for TDRSS. 
Measurement Residuals by Tracker  Displays measurement, residual, predicted sigma, ratio of residual to sigma, and the reason for rejecting the measurement, if any. Display is chronological, grouped by tracker. Valid for the filter. 
Measurement Residuals GPS  Supplements the Measurement Residuals report with the identity of the PRN(s) being tracked. 
Measurement Residuals TDRSS  Supplements the Measurement Residuals with the tracking strand for all facilities and satellites participating in the multilegged TDRSS measurement. 
Measurement Summary  Displays passbypass counts of measurements found in selected tracking data files. Valid for any standard tracking data file type. 
Measurement Summary by Altitude  The measurement update times are superimposed on a graph of satellite altitude. Altitude is computed using the satellite orbit estimate and a spherical earth. Valid for simulator, filter, smoother, and VLS. 
Measurement Summary by Sat  Counts the measurements in the tracking data files, tabulated by satellite. Valid for any standard tracking data file type. 
Measurement Summary by Sat and Track  Displays a count of measurements found in selected tracking data files, organized by tracker within satellite. Useful for evaluating multisatellite data files. Valid for any standard tracking data file type. 
Measurement Summary by Track and Sat  Displays a count of measurements found in selected tracking data files, organized by satellite within tracker. Useful for evaluating multisatellite data files. Valid for any standard tracking data file type. 
Measurement Summary by Tracker  Displays a count of measurements found in selected tracking data files, organized by tracker. Valid for any standard tracking data file type. 
Measurement Summary by Type  Displays a count of measurements found in selected tracking data files, organized by measurement type. Valid for any standard tracking data file type. 
Measurement Times by Sat  Graphs the times measurements where available and sorted by satellite. 
Measurement Times by Tracker  Graphs the times measurements where available and sorted by tracker. 
Measurement Times by Type  Graphs the times measurements where available and sorted by measurement type. 
Measurements  Lists the measurements in the measurements file. Valid for any standard tracking data file type. 
Measurements By Strand  Same as the Measurements report except that the grouping is by the complete tracking strand instead of just the (satellite, tracker). Useful for TDRSS. 
Measurements with Summary  Lists and summarizes the measurements in the measurements file, organized by pass, and measurement type within each pass. Valid for any standard tracking data file type. 
Observer Position  This report style is a special report for B3, Types 8 and 9 observations for Space Based angles data, where the observing platform ECF position is reported as part of the observation. This report style simply displays the observer as reported in the B3 observation. 
Pos Consistency  Graphs the FilterSmoother Consistency Test value and statistic for R, I and C position coordinates. Valid for differences generated by State Difference Tool, found on the LaunchPad Utilities tab. 
Pos Consistency Tests  Tabulates FilterSmoother position differences, sigma differences, and Consistency Test for R, I and C coordinates. Valid for differences generated by State Difference Tool, found on the LaunchPad Utilities tab. 
Pos Vel Uncertainty  Tabulate the position and velocity uncertainty, taken from the covariance. There are separate graph styles for 1sigma (0.68p), 2sigma(0.95p), and 3sigma(0.99p) uncertainties. Valid for filter and smoother. 
Position Uncertainty  Graphs the 0.95P position uncertainty, taken from the covariance. Valid for filter and smoother. 
Rejected Meas Residuals  Tabulates rejected residuals. Includes measurement, residual, sigma, test statistic, and reason for rejection. Valid for the filter. 
Residual Ratios  Graphs normalized residuals, where the normalized residual is the residual divided by the measurement error rootvariance. Normalizing is useful to display residual behavior of multiple measurement types on one graph. Valid for filter. 
Residual Ratio QQ  A QQplot of residual ratios with Royston acceptance boundaries. Note that "Q" stands for "Quantile". The filter residual ratio quantile points are plotted against the same test quantile from a Normal distribution. Distinction between a Normal distribution and a NonNormal distribution, for a particular level of significance, is achieved if all the filter residual ratio quantile points stay within the acceptance boundaries. This predefined product style plots two acceptance boundaries, one with a significance level of 0.995 and the other with a significance level of 0.9545 (roughly "3 sigma" and "2 sigma" respectively). 
Residual Summary  Generates statistics for measurement residuals, including mean, RMS about zero and RMS about the mean. Omits rejected measurements. Valid for the filter. 
Residuals  Graphs residuals with +/ 3s bounds. Valid for the filter. 
Residuals by Azimuth Angle  Graphs the residuals as a function of the azimuth angle. This is useful for checking to see if there are azimuth dependent biases or white noise variation. 
Residuals by Elevation Angle  Graphs the residuals as a function of the elevation angle. This is useful for checking to see if there are elevation dependent biases or white noise variation. 
Residuals by Range  Graphs the residuals as a function of the range. This is useful for checking to see if there are range dependent biases or white noise variation. 
Residuals by Time of Day  Graphs the residuals as a function of the time of day (UTC time scale). This is useful for checking to see if there are time dependent biases or white noise variation. 
Residuals with Bias  Graphs residuals with +/ 3s bounds and includes the bias estimate. Valid for the filter. 
Retroreflector Delay  Graphs the corrections to the retroreflector delay used in processing SLR measurements. 
RIC SigmaCorrelation Matrices  Tabulates satellite position / velocity covariances in sigmacorrelation form. Valid for filter and smoother. 
Satellite Classical Element Uncertainties  Report style which tabulates satellite estimated orbit element error sigma. Valid for filter and smoother. Note that the transformation for the uncertainties from Cartesian to Classical Elements has singularities at e=0, and i=0 or 180 deg. This transformation will be degraded near the singularity points. 
Satellite Classical Element Uncertainties (a e)  Graph style which displays the satellite estimated semimajor axis (a), and eccentricity (e) 0.95 error bound. The semimajor axis is displayed using the primary yaxis, while the eccentricity is displayed using the secondary yaxis. Valid for filter and smoother. 
Satellite Classical Element Uncertainties (i)  Graph style which displays the satellite estimated inclination (i), and 0.95 error bound. 
Satellite Classical Elements  Tabulates satellite position / velocity in orbital element form. Valid for filter and smoother. 
Satellite Classical Elements Plus  Displays a satellite's true anomaly and orbit period in addition to the other Satellite Classical Elements. 
Satellite NonOrbit Parameters  Tabulates density estimate, SRP coefficient estimate and transponder bias estimate and the corresponding sigmas for each. Valid for filter and smoother. 
Satellite Pos Vel  Tabulates satellite position / velocity in Cartesian ECI coordinates. Multiple points at same time tag indicate each measurement correction. Valid for filter and smoother. 
Satellite Pos Vel (Corrected)  Displays satellite position and velocity at measurement times. Valid for filter and smoother. 
Satellite Pos Vel (Predicted)  Tabulates position and velocity in Cartesian ECI Coordinates. Similar to Satellite Position Velocity except points due to measurement update are not tabulated. Valid for filter and smoother. 
Satellite Summary  Displays the final orbit state for the filter, giving epoch, position and velocity, orbit elements, density correction estimate, SRP correction estimate, and transponder bias estimate, and final orbit covariance. This file is complimented by Tracker Summary. Valid only for the filter. 
Sim Atmosphere Density Estimate  Displays atmospheric density estimates (or deviates if simulator) (Dr/r). Valid for simulator, filter, and smoother. 
Sim Measurement Noise  Displays simulated measurement deviates and corresponding sigma in natural measurement units. Only useful for simulator. 
Sim Measurement Noise Normalized  Displays simulated measurement deviates and corresponding sigma normalized to units of multiples of sigma. Only useful for simulator. 
Sim Measurements  Displays the deviates added to each measurement for constant bias, Gauss Markov bias and noise. Only useful for simulator. 
Sim Sat Initial State  Tabulates the deviation of initial conditions for orbit as well as density, solar pressure and transponder. Report displays the original values and deviated values. The actual deviates are tabulated in Sim Sat Perts. Only useful for simulator. 
Sim Sat NonOrbit Parameters  Tabulates timevarying deviates applied to density, solar pressure and transponder vs. time. Only useful for simulator. 
Sim Sat Perts  Tabulates the initial condition deviates assigned to orbit parameters as well as density, solar pressure and transponder by simulator. This report is the compliment of the Sim Sat Initial State report, which displays the "before" and "after". Only useful for simulator. 
Sim SRP Estimate  Displays the estimated / deviated solar radiation pressure coefficient. Valid for simulator, filter, and smoother. 
Sim Tracker Initial State  Tabulates the initial state deviates assigned to trackers, organized by tracker and measurement type. Includes Gauss Markov deviate, bias and the initial sigma for the Gauss Markov state. 
Sim Transponder Bias  Displays transponder deviate / estimate. Valid for simulator, filter and smoother. 
SRP Estimate  Displays solar pressure parameter estimate and 0.95P bounds, derived from the state covariance. Valid for filter or smoother. 
SRP Plugin States  Supports Solar Pressure Reflectance Plugin Model. Displays solar pressure parameter estimate and 0.95P bounds, derived from the state covariance for all parameters in the model. Valid for filter, smoother, and simulator. If simulator the estimate reflects the "perturbation". 
SRP States (Scale)  An example custom style to support the Solar Pressure Reflectance Plugin Model. Displays, for the selected parameter only, the solar pressure parameter estimate and 0.95P bounds, derived from the state covariance. Valid for filter, smoother, and simulator. If simulator, the estimate reflects the "perturbation". In this particular case the selected parameter name is "Scale". 
SRP States (Y Bias)  Similar to SRP States (Scale), except that in this case the selected parameter name is "Y Bias". 
Tracker Bias Consistency  Graphs the FilterSmoother Consistency Test value and statistic for the selected tracker bias(es). Valid for differences generated by State Difference Tool. 
Tracker Measurement Bias  Displays tracker measurement bias and 0.95P bounds. Valid for filter and smoother. 
Tracker Measurement Bias State History  The report style tabulates the tracker measurement bias nominal value, correction estimate and total bias estimate. The graph style displays the tracker measurement bias correction estimate and 0.95P error bounds, derived from the state covariance. Valid for filter and smoother. 
Tracker Summary  Tabulates final tracker state estimate and covariance. This graph compliments Satellite Summary. Valid only for the filter. 
Transponder Bias  Displays transponder bias estimate and 2sigma error bounds. Valid for filter or smoother. 
Troposphere Measurement Corrections  Displays troposphere refraction corrections to the modeled measurement and the uncertainty (1 sigma) assigned to the correction. Valid for the filter. 
Troposphere Bias  Displays troposphere zenith bias estimate and 2sigma error bounds. Valid for filter or smoother. 
True Anomaly  Tabulates satellite true anomaly. Valid for filter and smoother. 
Vel Consistency  Graphs the FilterSmoother Consistency Test value and statistic for velocity in R, I and C coordinates. Valid for differences generated by State Difference Tool, found on the LaunchPad Utilities tab. 
Vel Consistency Test  Tabulates FilterSmoother velocity differences, sigma differences and Consistency Test for R, I and C coordinates. Valid for differences generated by State Difference Tool, found on the LaunchPad Utilities tab. 
Velocity Uncertainty  Graphs the 0.95P velocity uncertainty, taken from the covariance. Valid for filter and smoother. 
Note: Other product styles may have been added since this page was last edited. Check the Product Styles area in the Static Product Builder for the most current list.
ODTK 6.5