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Watson Industries, Inc. 

 

DMS-EGP02 Rev A 03/28/2008 

 

2. 

An “I” or “i” sets the unit to Inertial mode.  This is the default mode at power up and is the 
normal operating mode.  Switching to this mode clears the Reference Command mode.  
This will also disable the logic input Reference Command and Free Mode Command until 
the next time the unit is powered up.  Double spacebar at initialization is required for access 
to this command. 

 

 

3. 

An “F” or “f” will disconnect the references from the attitude system and is the Free Mode 
Command.  Free mode is used to make the system ignore the references during high 
maneuvers and brief disturbances.  This mode is not intended for use except in brief 
intervals, since errors will grow geometrically.  This will also disable the logic input 
Reference Command and Free Mode Command until the next time the unit is powered up. 
This command does not require a double space bar at initialization to be in effect. 

 
4.  

An “H” or “h” will remove bias correction from the system and is the Hold Mode 
Command. This mode is useful is highly dynamic situations that may last for a few minutes.  
Hold mode should not be used for more than a few minutes, because errors can accumulate. 
This command does not require a double space bar at initialization to be in effect.   

 
 

5. 

A “K” or “k” will clear the Free Mode Command and the Hold Mode Command. 

 

6. 

An “!”  will reinitialize the unit.  Further, the access to initialization is inhibited such that a 
spacebar command must be sent within 2.5 seconds of the “!” command for initialization to 
be engaged.  This command does not require a double space bar at initialization to be in 
effect. 

 

There are two output format commands: “_” for decimal output and “^” for binary.  See second part 
of Appendix A for more information on changing output formats.  There are several interface 
commands as well:  “:” will toggle the output to send a frame of data upon receiving any non-
command character and “+” will toggle the output for no output data.    These and other changes 
can be made permanent by keying in the quote (“) character.  Double spacebar at initialization is 
required for access to all of these commands. 

 

The “&” command calls a menu which allows any of several parameters to be set.  From this menu, 
the user can change system time constants, data channels for serial output, heading source, velocity 
source and baud rate.  Double spacebar at initialization is required for access to this command. 

 

The commands “~”, “@”, “#”, “$”, ‘(“, “)”, “{“, “}”, “|”, “<”, “>” and “?” are used by the Watson 
factory to calibrate the unit and should be used only with the assistance of the factory.   If an 
undesired function is called, a “Q”, and sometimes Escape or a Delete will interrupt the command 
and return to operation with the least disturbance to the system.  All other unspecified characters 
such as carriage return, line feed and space are ignored by the system. 

 

If there are problems with the system “hanging up” during the binary output mode, check for cross-
talk between the serial transmit and receive line in your installation.   In addition, check to see that 
the communications program used is not sending an echo. This will not happen in the decimal or 
hexadecimal modes because command characters recognized by the system are not produced in 
those modes. Please note that the signal and power ground are isolated from one another. 
 
 
 

Summary of Contents for DMS-EGP02

Page 1: ...A 03 28 2008 1 DYNAMIC MEASUREMENT SYSTEM OWNER S MANUAL PART NUMBER DMS EGP02 GPS Module Dual Antenna System WATSON INDUSTRIES INC 3041 MELBY ROAD EAU CLAIRE WI 54703 Phone 715 839 0628 FAX 715 839...

Page 2: ...2 14 Figure 3 Antenna Dimensions 15 7 Warning 15 8 Appendix A 18 Determining and Setting Output Channels 19 Setting Output Format 20 Setting Heading Mode 20 Setting Velocity Mode 21 9 Appendix B 22 10...

Page 3: ...ion Calibration is achieved by using the maintenance software to store data in non volatile memory within the DMS The DMS EGP02 differs from a standard DMS with the addition of a Dual antenna GPS syst...

Page 4: ...tellites The Fore antenna is placed meter ahead of the Aft Antenna on a line parallel to the axis of the vehicle Caution The GPS heading accuracy is directly related to the accuracy of the antenna pla...

Page 5: ...g structure is discussed later in the Interface section of this manual The DMS generates twelve different data items for output X Y and Z rates X Y and Z accelerations Bank Elevation and Heading and F...

Page 6: ...adjustments to the gyros It is intended for short term use only since leaving biases uncorrected will allow errors to accumulate over time The accumulating bias error will result in small attitude err...

Page 7: ...e for up to 9 99 g s 7 A six character string representing the Z axis acceleration starting with a or a followed by one digit a decimal point two digits and a space for up to 9 99 g s 8 A six characte...

Page 8: ...th no detectable effect on the resulting data The other output format available is a binary format In this mode the unit provides generally the same information as the decimal ASCII format but in a co...

Page 9: ...his command does not require a double space bar at initialization to be in effect There are two output format commands _ for decimal output and for binary See second part of Appendix A for more inform...

Page 10: ...al data output This allows the system to act as a data acquisition unit for other vehicle information such as engine RPM engine temperature fuel remaining altitude depth or any other important data Th...

Page 11: ...to 5VDC The pins are as follows a Initialization Resets all angle integrators The unit should be in a non accelerated condition if this command is given Leave pin open if not in use Ground to command...

Page 12: ...range Bandwidth 20 Hz Environmental Temperature Operating 30 C to 60 C Temperature Storage 55 C to 85 C Vibration Operating 5g rms 20 Hz to 2 kHz Vibration Survival 10g rms 20 Hz to 2 kHz Shock Surviv...

Page 13: ...A 03 28 2008 13 Figure 1 Up Position Receive from 9 pin connector This is non GPS mode Allows Keyboard commands to be input into the unit Down Position Receive from GPS module This is the GPS mode Ke...

Page 14: ...d 18 Y Axis Acceleration Analog Output 4 Shorted to pin 6 8 Coast Command 19 Z Axis Acceleration Analog Output 5 Ground 9 Ready 20 Forward Acceleration Analog Output 6 Shorted to pin 4 10 Initializati...

Page 15: ...Watson Industries Inc DMS EGP02 Rev A 03 28 2008 15 Figure 3 Antenna Dimensions Warning Rough handling dropping or miswiring this unit is likely to cause damage...

Page 16: ...ny warranty given by Watson Industries are products that have been subject to abuse misuse damage or accident that have been connected installed or adjusted contrary to the instructions furnished by s...

Page 17: ...628 Fax 715 839 8248 Email support watson gyro com All sensors returned under warranty will be repaired or replaced at the sole option of Watson Industries at no cost to the customer other than shippi...

Page 18: ...Rate 99 9 s 200 s Corrected Bank Pendulum simulated 179 9 180 Corrected Elevation Pendulum simulated 89 9 180 User Channel 1 9 99 VDC 10 VDC User Channel 2 9 99 VDC 10 VDC User Channel 3 9 99 VDC 10...

Page 19: ...e this will bring up the menu again Now type 2 to set up channels The following message will appear To proceed type Y or y Now each channel will come up one at a time For example Type Y or y to output...

Page 20: ...e up position so that the unit can receive computer commands Turn on unit Wait for the startup message to appear on display Hit the space bar twice within the first 5 seconds of turn on Sometimes it t...

Page 21: ...lection the default the next time you power the unit on type in double quote Setting Heading Calibration Hook the unit up to your computer s serial port Use a terminal program to interface with the un...

Page 22: ...angular displacement signals Careful note should be taken of the angles indicated in the reference mode The sensor should then be tipped on the pivot into the other stable position and the angle agai...

Page 23: ...the sensor at a 45 angle to the horizontal in pitch only taking care not to move the sensor at an angular rate of more than 100 sec The Forward Lateral and Vertical Acceleration outputs should not cha...

Page 24: ...rd This word is then shifted left to shift out the sign bit What remains is a signed fractional word with a resolution of 13 bits plus a sign bit DATA STREAM WORD 1 WORD 2 WORD 3 WORD 4 WORD N 0x0D Ca...

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