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Vlas Karpov
Vlas Karpov

GPS Tracker Parameter Editor V1.


Press the SOS button and keep on holding, then turn on thetracker, both of the two LED lights will be on and keep stable. Thetracker is now ready to be configured. Click the Read button toread all preset parameters.




GPS Tracker Parameter Editor V1.


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GPRS - Tick GPRS to enable GPRS tracking TCP/UDP - Choose TCP orUDP communication Tracker ID - Set ID for the tracker. For example:888888 APN - Name of your APN provider APN Account and APN password-Input user name and password if any. If not, leave these two itemsblank (for the APN, APN account, APN password, pls check with yoursim card operator) IP and Port - Input the IP and Port of yourserver Interval - Set interval for GPRS tracking


Password - Set or change users password for sending SMScommands. Prefix (area code) - Be advised caution in this setting.Normally, your country code (for example in China it is +86) willbe automatically added and displayed prior to a phone number whensending SMS. In this case, you should leave this column blank. Ifthe country code is not added you are required to input the countrycode here, for example, +86. Wiretapping - Set phone number forvoice surveillance / wiretapping (listen only). Logging - Setinterval for logging Power Saving - Set power saving mode whentracker is inactive. In power saving mode, GPS stops working andGSM enters standby mode. For example, if it is set 10, thetracker


Over Speed - Set over speed alert Time Zone - Set timedifference in minute to GMT (default time zone is GMT). For thoseahead of GMT just input the time difference in minute. For example,120; For those behind GMT, - is required. For example, -120.Geofence - Nul: to disable geo-fencing function; Out: to setgeo-fencing alert when tracker exits geo-fencing area; In: to setgeo-fencing alert when tracker enters geo-fencing area.


Call for SMS Blank: Close location report function when a callis made to the tracker; Ticked: Open location report function toget position SMS by calling the tracker Blank: Analyze position SMSformat to be read easily. For example: Latitude = 22 32 36.63NLongitude = 114 04 57.37E, Speed = 2.6854Km/h, 2008-12-24, 01:50Ticked, Location SMS format is in NMEA 0183 Format. For example:$GPRMC,072414.000,V,3114.3763,N,12131.3255,E,0.00,0.00,050805,*00Auto Shut Blank: The tracker does NOT automatically hang up whenone call incoming. Ticked: The tracker hangs up after 45 rings ofan incoming call String Format


Tracker-on Blank: The tracker does NOT send SMS to SOS presetnumber when it is turned on Ticked: the tracker sends one SMS toSOS preset number when it is turned on. Blind Area Blank: Thetracker does NOT send SMS to the SOS preset number when itenters/exits GPS blind area. Ticked: The tracker sends alert SMS tothe SOS preset number when it enters/exits GPS blind area. LED OffBlank: The LED light(s) in normal flashing status when the trackerworks Ticked: Turn off the LED light(s) when the tracker isworking.


Write - There are two functions for this button. If you haveseveral items to be set, you dont have to click the Apply buttonone by one. When you finish all inputs, click Write button to applyall the settings to the tracker. Or if you want to apply samesettings to another tracker, click Write button when a new


Auto -when configuration is complete and you need to apply sameparameters to other trackers (for bulk configuration), you cansimply tick Auto to make an automatic configuration. After anothertracker is connected and turned on by pressing and holding SOSbutton, immediately it will be automatically configured.


You can change and check the parameters for another version: jQuery.getJSON("../_static/parameters-Copter.json", , function(json) $.each(json, function(key, value) $('.selectpicker').append('' + key + ''); ););


This can be used to force an action on flight termination. Normally this is handled by an external failsafe board, but you can setup ArduPilot to handle it here. Please consult the wiki for more information on the possible values of the parameter


This enables the dual loss termination part of the AFS system. If this parameter is 1 and both GPS and the ground control station fail simultaneously, this will be considered a "dual loss" and cause termination.


This controls whether to use dead-reckoning or GPS based navigation. If set to 0 then the GPS won't be used for navigation, and only dead reckoning will be used. A value of zero should never be used for normal flight. Currently this affects only the DCM-based AHRS: the EKF uses GPS according to its own parameters. A value of 2 means to use GPS for height as well as position - both in DCM estimation and when determining altitude-above-home.


Checks prior to arming motor. This is a bitmask of checks that will be performed before allowing arming. For most users it is recommended to leave this at the default of 1 (all checks enabled). You can select whatever checks you prefer by adding together the values of each check type to set this parameter. For example, to only allow arming when you have GPS lock and no RC failsafe you would set ARMING_CHECK to 72.


This parameter allows you to control whether the order in which the tubes are attached to your pitot tube matters. If you set this to 0 then the first (often the top) connector on the sensor needs to be the stagnation pressure (the pressure at the tip of the pitot tube). If set to 1 then the second (often the bottom) connector needs to be the stagnation pressure. If set to 2 (the default) then the airspeed driver will accept either order. The reason you may wish to specify the order is it will allow your airspeed sensor to detect if the aircraft is receiving excessive pressure on the static port compared to the stagnation port such as during a stall, which would otherwise be seen as a positive airspeed.


This parameter allows you to skip airspeed offset calibration on startup, instead using the offset from the last calibration. This may be desirable if the offset variance between flights for your sensor is low and you want to avoid having to cover the pitot tube on each boot.


User provided ambient ground temperature in degrees Celsius. This is used to improve the calculation of the altitude the vehicle is at. This parameter is not persistent and will be reset to 0 every time the vehicle is rebooted. A value of 0 means use the internal measurement ambient temperature.


User provided field elevation in meters. This is used to improve the calculation of the altitude the vehicle is at. This parameter is not persistent and will be reset to 0 every time the vehicle is rebooted. Changes to this parameter will only be used when disarmed. A value of 0 means the EKF origin height is used for takeoff height above sea level.


This is the maximum acceptable altitude discrepancy between GPS altitude and barometric presssure altitude calculated against a standard atmosphere for arming checks to pass. If you are getting an arming error due to this parameter then you may have a faulty or substituted barometer. A common issue is vendors replacing a MS5611 in a "Pixhawk" with a MS5607. If you have that issue then please see BARO_OPTIONS parameter to force the MS5611 to be treated as a MS5607. This check is disabled if the value is zero.


This is the ratio of static pressure error to dynamic pressure generated by a positive wind relative velocity along the X body axis. If the baro height estimate rises during forwards flight, then this will be a negative number. Multirotors can use this feature only if using EKF3 and if the EK3_DRAG_BCOEF_X and EK3_DRAG_BCOEF_Y parameters have been tuned.


This is the ratio of static pressure error to dynamic pressure generated by a negative wind relative velocity along the X body axis. If the baro height estimate rises during backwards flight, then this will be a negative number. Multirotors can use this feature only if using EKF3 and if the EK3_DRAG_BCOEF_X and EK3_DRAG_BCOEF_Y parameters have been tuned.


This is the ratio of static pressure error to dynamic pressure generated by a positive wind relative velocity along the Y body axis. If the baro height estimate rises during sideways flight to the right, then this should be a negative number. Multirotors can use this feature only if using EKF3 and if the EK3_DRAG_BCOEF_X and EK3_DRAG_BCOEF_Y parameters have been tuned.


This is the ratio of static pressure error to dynamic pressure generated by a negative wind relative velocity along the Y body axis. If the baro height estimate rises during sideways flight to the left, then this should be a negative number. Multirotors can use this feature only if using EKF3 and if the EK3_DRAG_BCOEF_X and EK3_DRAG_BCOEF_Y parameters have been tuned. 350c69d7ab


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