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WinFrog User’s Guide - Appendix C – GPS/MX 9400 

Page 15 of 

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GDOP

 – Geometric Dilution of Precision. GDOP is a numerical value that serves as 

a measure of the effect of the satellite constellation’s geometry on the derived 
positional accuracy. In other words, the GPS receiver’s measurement accuracy is 
multiplied by the GDOP value to derive the overall positional accuracy of the GPS 
receiver (including the three positional dimensions and clock offset). If the GDOP 
mask is set to On and the calculated GDOP exceeds the entered value, WinFrog will 
not compute a position solution using pseudoranges. If the Calculations window is 
enabled, an alarm will sound to indicate that the GDOP has been exceeded. 
 

VDOP

 

 Vertical Dilution of Precision. This parameter is also calculated from satellite 

geometry and gives an indication of the expected accuracy of the vertical component 
of the GPS position solution. If the VDOP mask is set to On and the calculated 
VDOP exceeds the entered value, WinFrog will automatically initiate 2D or fixed 
height mode using either the last valid calculated height or the height entered in the 
Antenna Height

 Ellipsoid Height 

field. If the Calculations window is enabled, an 

alarm will sound to indicate that the VDOP has been exceeded. 
 

Elev. Cutoff

 – (Elevation Angle Cutoff). WinFrog will not use measurements from 

any satellites with elevation angles below the angular value input in the Elevation 
Angle Cutoff field. Any satellites not used in the pseudorange position calculations 
are indicated in the Calculations window by a change of color.  
 

Min SN

 

 Minimum Signal to Noise. This field is used to set the minimum signal to 

noise ratio for the pseudorange calculations. If a satellite’s signal to noise ratio falls 
below the entered value, the satellite will not be used in position computation by 
WinFrog. Satellites not used in the position computation due to low signal to noise 
values are indicated in the Calculations window by a change of color.  
 

Max Res

 

 Maximum Measurement Residual. WinFrog will not use any satellite 

measurement with a residual greater than the Maximum Measurement Residual in 
its pseudorange position computations. Satellites not used in the position 
computation due to measurement residuals are indicated in the Calculations window 
by a change of color.  
 

Max RTCM Age

 

 Maximum RTCM Differential Correction Age. This parameter sets 

the maximum latency of real time differential corrections for pseudoranges. If the 
maximum latency is exceeded, WinFrog will not apply the corrections from that 
RTCM source. To indicate this condition, the 

STAT

 light in the Position

 

portion of the 

Calculations window will turn yellow. Click on the 

ACK

 button to acknowledge this 

alarm.  

 

 

Test: 

Click this button to open the

 GPS Solution Statistical Testing

 dialog box, as seen 

below. 
 

Summary of Contents for MX9400N

Page 1: ...ts to generate three dimensional positions The MX9400 can accept standard RTCM SC 104 input to generate and output a differentially corrected position The MX9400 can also output pseudorange ephemeris and time and date information which can be used by WinFrog s GPS Calculations extension module to internally calculate a GPS position The MX9400 utilizes 4 serial interface ports that communicate via ...

Page 2: ...NS WINFROG I O DEVICES EDIT I O Serial Configurable Parameters The MX9400 is added to WinFrog from the GPS device group Configure the Device I O Parameters dialog box for the appropriate Baud Rate Data Bits Stop Bits Parity and Comm Port These selections refer only to the WinFrog computer port that is connected to the MX9400 CDU port i e Port 1 on the MX9400 see below for more on the MX9400 s port...

Page 3: ...data output through the Data Logging port Position GPGLL This is a standard NMEA format type message containing GPS Latitude Longitude data output through the Data Logging port Speed GPVTG This is a standard NMEA format type message containing Track and Speed Over Ground data output through the Data Logging port Residuals GPGRS This is a standard NMEA format type message containing GPS Residual da...

Page 4: ...n select to send only the GPGGA preferred or the GPGLL item As defined above by default these NMEA messages are output from the Data Logging port i e port 4 In order to interface to the MX9400 through just one of its ports you must reassign this output to another port port 1 Port 1 must be interfaced to WinFrog in order for the CDU commands to be received so this is the port of choice To reassign ...

Page 5: ...configuration is typical of that used in most WinFrog operations If you are only using the MX9400 s internally calculated position you need only select a Position GPGGA or GPGLL item Once this dialog box is correctly configured click the OK button WinFrog sends the configuration commands to the MX9400 and closes the dialog To reconfigure any one of these options select the MX9400 device in the I O...

Page 6: ...es in order to calculate a valid 3 dimension position Fixed This mode selection fixes the MX9400 s height to the ellipsoidal height value entered in the Ellipsoid Height box In this mode the MX9400 is able to calculate valid positions using a minimum of three satellites Auto Last Height The MX9400 will calculate a valid 3D position if four or more satellites are available If only three satellites ...

Page 7: ...hin this box There are four different DGPS modes Off Generate Auto and On Off The MX9400 will not use differential corrections in its position computations for that device even if they are available Instead it will compute only a single point GPS solution Generate The MX9400 will generate base station corrections based on the GPS data being received and the position input at the top of the window ...

Page 8: ... The MX9400 can also output raw Pseudorange and Ephemeris data for WinFrog to calculate the position itself using WinFrog s GPS Calculations extension module This is setup by adding both the GPS MX9400 PSEUDORANGE and the GPS MX9400 EPHEMERIS data items to the vehicle s device list Additionally a Time Date message can also be output to provide WinFrog with more precise timing information Add the G...

Page 9: ...ositioning will go to dead reckoning if dead reckoning is turned on You must manually change a Secondary device to Primary in order for the data to be utilized Use For Heading Calculations Select this checkbox if the device is to be used in conjunction with another GPS device for determination of the heading of the vessel Graphics If On is selected a labeled square will show the raw offset but unf...

Page 10: ...ssociated with the GPS unit being used For all other applications the Code entry must be set to 0 Offsets Offsets are required to associate the GPS antenna position with the vessel s Common Reference Point i e CRP The offsets are applied from CRP of the vehicle to the GPS antenna location Forward Offsets are entered as positive values Aft Offsets are entered as negative values Starboard Offsets ar...

Page 11: ...hicles position solution that device s position will simply be received and monitored Note that in the case of Primary device failure WinFrog will not automatically use the Secondary devices for the vehicle position computation Instead it will start dead reckoning if dead reckoning is turned on You must manually change a secondary device to primary status if you want to utilize the data coming fro...

Page 12: ...WinFrog requires a minimum of four satellites to be visible Fixed Select this option to fix the GPS antenna ellipsoid height to the value entered in the Ellipsoid Height field In this mode WinFrog is able to calculate valid positions using a minimum of three satellites Auto Last Height If this mode is selected WinFrog will calculate a 3D position if four or more satellites are available If only th...

Page 13: ...othing utilizes the GPS receiver s observations of the GPS satellite s carrier signals Because the GPS L1 frequency has a wavelength of only 19 cm measurements made using this signal will provide higher accuracy than measurements made on the C A code message modulated onto the L1 signal Note however that since the carrier phase position is derived from the C A code position it does not offer an im...

Page 14: ... Ref position and all individual solutions Data The Calculations window will show the results of the GPS Calculations including the Multi Ref position and data related to each individual carrier phase solution when Phase Smoothing is enabled Statistics The Calculations window will show the results of the GPS Calculations including the Multi Ref position and statistical data related to each individ...

Page 15: ... will not use measurements from any satellites with elevation angles below the angular value input in the Elevation Angle Cutoff field Any satellites not used in the pseudorange position calculations are indicated in the Calculations window by a change of color Min SN Minimum Signal to Noise This field is used to set the minimum signal to noise ratio for the pseudorange calculations If a satellite...

Page 16: ...ion approaches the minimum required it is unlikely that WinFrog will ever have to stop the exclusion of data due to insufficient satellites Nonetheless WinFrog still checks for this condition Caution should be exercised when using this option If the vessel is too far away from the selected reference stations and or there are few satellites in common with the vessel and the reference station s the ...

Page 17: ...ns are utilized in the solution each with the same Relative Standard Deviation The individual station method is preferable as it allows you to remove or de weight solutions that may not agree with the weighted mean solution If this method is used you should add the RTCM data item to the vehicle s device list once for each solution then edit that solution entering the proper code and coordinates Fo...

Page 18: ...ted from the data Monitor Reference Station is simply monitored by WinFrog and is not used in the Multi Ref position This solution will appear in yellow text in WinFrog s Calculations window Rel Std Dev This value defines the relative standard deviation of this solution as compared to the other solutions used in the Multi Ref position Equal Rel Std Dev values indicate that all individual solutions...

Page 19: ...ce before WinFrog resets its clock This should not be set too small or the clock will constantly be re setting A tolerance of 50 ms for a 1PPS pulse results in the resetting of the clock approximately every 5 6 minutes WinFrog monitors the variation between the UTC time and the WinFrog clock using a fading history of the last 20 samples of the variation between the WinFrog clock synchronization ti...

Page 20: ...lowing information is displayed Status Displays the data type status On Off and the associated device status Sync d at Displays the time the WinFrog clock was last adjusted Computer time WinFrog clock time stamp of last synchronization data input UTC time UTC time from device of last synchronization data input Raw Delta The difference between the UTC and associated WinFrog time stamp UTC WinFrog f...

Page 21: ...top proprietary outputs on CDU port PMVXG 026 1 turn off equip port output PMVXG 007 412 1 5 turn psn output to CDU port PMVXG 007 100 1 2 turn SV trking status output to CDU port PMVXG 007 000 1 5 turn RCVR status output to CDU port PMVXG 001 d 3lf 3lf 1lf c 0lf tempHgtMode PMVXG 053 d 0lf 0 6 d 0 0 0 tempDgpsCode PMVXG 034 d 0 0 1lf d 0 tempBitR Rate of 50 1 100 2 or 200 3 Items to Send Messages...

Page 22: ...Measurement Accuracy 10cm code single epoch 5mm phase Connectors Multiport I F DB25S Time SMB Jack receptacle Event Input SMB Jack receptacle Antenna SMA Jack receptacle Power DC Power Jack 0 1 dia Navigation Mode Operating Modes 2D or 3D DGPS GPS or auto selection DGPS Input RTCM SC 104 format Time to First Fix 1 minute typical Accuracy Position 30 cm RMS 15 cm RMS AccucodeTM Velocity 05 m s RMS ...

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