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Watson Industries, Inc. 

 

DMS-EGP02 Rev A 03/28/2008 

 

Operation

 

Initialization 

Ideally, the DMS should be stationary and level when it is turned on.  If not, the sensor readings 
may not be accurate after initialization.  The time required for the initialization process is not the 
same for every type of DMS, but typically takes 4 to 5 seconds.  During this time, a message is sent 
from the unit via the RS-232 serial link.  This message gives information about the DMS such as 
the full model number, serial number, and software revision.  The message can be read by using a 
terminal program or by using the terminal mode of Watson Industries’ communication software. 

 
 

The DMS can also be “re-initialized” after it has been turned on. This is especially useful if the 
sensor has been used in severe maneuvers that have over-ranged the angular rate sensors and 
caused significant errors to accumulate.  Sometimes re-initializing the unit will allow for a faster 
recovery than waiting for the error correction routines to correct the sensor readings.  There are 
several ways to re-initialize the DMS. For more information, see the Interface section of this 
manual.  Please note that in order to use the GPS mode of this unit, the switch must be in the down 
position when the unit is initialized or re-initialized (See Figure 1).   

Normal Operation 

During normal operation, the DMS will output highly accurate inertial data for the user to interpret. 
This data is transmitted in several different ways. The most common way to acquire data from the 
DMS is to use the RS-232 serial output.  There are two RS-232 output formats: decimal and binary.  
The exact formatting 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 Forward, Lateral, and Vertical Accelerations.  Any combination of 
these data items can be selected for transmission via the RS-232 serial link. The DMS also has 
analog outputs (see Interface section) that can be used to send data to the user. 

 

In normal operation, the DMS takes data from its internal rate sensors and integrates in a closed 
loop system, with the accelerometers as a long-term reference, to generate Bank, Elevation and 
Heading data.  In most cases, these algorithms provide for very stable and accurate output signals; 
However, the user should be aware that exceeding the normal ranges of the sensors will affect 
accuracy.  For example, while custom DMS units may have differing ranges, the gyros in a typical 
DMS have a maximum rate of 100

°

/s.  Care should be taken not to exceed this rate because the 

closed loop system will receive inaccurate data. This will result in errors in the angle output 
signals. 

 

While this DMS is "all attitude", the accuracy deteriorates rapidly when its forward direction is 
within about 5 degrees of vertical. Operation for any extended period of time in this orientation is 
not recommended.  If these few operational precautions are observed, the DMS should provide 
very accurate data for a wide variety of applications. 

Special Operation Modes 

Reference Mode 
This mode is usually used for calibration or diagnostics. When in reference mode, the DMS will 
output data generated directly from the sensor reference signals rather than as a product of the 
closed loop integration used for normal operation. This mode provides sensor information similar 
to normal operation mode with the following differences: 

 

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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