WATSON INDUSTRIES DMS-S605 Скачать руководство пользователя страница 8

Watson Industries, Inc. 

 

DMS-SGP02 Rev K 03/22/2018 

 

Example: 
 

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161409.9 

-000.8 

+00.1 

273.4 

+028.9 

+44.86405 

-091.46836 

00894 

 

<CR> 

       

 

 

 

 

 

 

 

 

 

 

 

 

 

    

 

 

 

 

 

 

 
 
(1) 

 

UTC 

(2) 

Bank 
angle 

(3) 

Elev. 

angle 

(4) 

Head. 

angle 

(5) 

 
Velocity        

(6) 

 

Latitude 

(7) 

 

Longitude 

(8) 

 

Altitude 

(9) 

 

 
 

(10) 

 

space 

space 

space 

space 

space 

space 

space 

space 

space 

 

 
 

 

The string transmission rate can be improved by reducing the amount of information (data items) 
transmitted.  The data items transmitted can be changed by using special commands to modify the 
EEPROM of the unit (see Appendix A). In addition, more channels are available for output (see 
Appendix A). 

 

The system is protected from inadvertent write-over of the EEPROM by requiring two spacebar 
commands during the initialization interval to access the EEPROM or related functions.  

 

The baud rate may be changed from the nominal value of 9600 baud by modifying the default 
value in the EEPROM of the unit to 38.4K, 19.2K, or 4800 baud.  

 

A text header is sent by the DMS during initializations that identifies the unit by part number and 
by serial number and gives the date of last calibration. This whole message can be temporarily (or 
as a default) suppressed or restored by a “*” command from the interfacing computer.

 

 

Data transmission sent by the DMS can also be suppressed or restored by a “+” command from the 
interfacing computer.  This is used when only analog data is used as a noise reduction measure. 

 

The error over-range condition is indicated by the use of a lower case “i”, “t”, “g” or “r” when the 
calculated attitude or heading error exceeds the ranges listed above.  Internal functions that require 
these error values are disabled while the condition exists.  The system will continue to operate in an 
extended time constant mode with a low level of error accumulation until the condition is cleared.  
While maneuvering the vehicle, occasional blips of this condition are expected with 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 compact binary message.  In this format, 
there are nominally 13 words sent that represent 6 fourteen-bit output channels followed by a 
carriage return.  Again, the channels may be reduced to improve the update rate by using special 
commands to modify the EEPROM of the unit.  This format is for highly experienced users only.  
Consult the factory for further details.

 

 
RS-232 Input Commands 
The RS-232 input commands are provided for the purpose of unit test and installation set-up. Use 
the same parameters that are used as for the output (9600 baud ASCII nominal, or as reset in the 
units EEPROM).   
 
Note: Many commands require command or “Double spacebar mode” in order to access them. For 
more information on how to activate Command Mode, see the instructions in Appendix A. 
 
These commands are available to the user (others are used at the factory for alignment and 
calibration).   
1. 

An “R” or “r” will set the outputs (analog and serial) to their Reference Command modes, 
replacing the Inertial mode.  This will also disable the logic input Reference Command and 

Содержание DMS-S605

Страница 1: ...22 2018 1 DYNAMIC MEASUREMENT SYSTEM OWNER S MANUAL PART NUMBER DMS SGP02 Gyro System With GPS Module Dual Antennas WATSON INDUSTRIES INC 3035 MELBY STREET EAU CLAIRE WI 54703 Phone 715 839 0628 FAX 7...

Страница 2: ...7 8 Appendix A 18 Activating Command Mode Double Spacebar Mode 20 Determining Output Channels 20 Setting Output Channels 20 Setting Output Format 21 Setting Heading Mode 21 Setting Velocity Mode 22 Se...

Страница 3: ...tion is achieved by using the maintenance software to store data in non volatile memory within the DMS The DMS SGP02 differs from a standard DMS with the addition of a Dual Antenna GPS System This all...

Страница 4: ...nsor allows antenna spacing in millimeters from 0 3m up to 5m See Appendix A The larger the spacing the more accurate the GPS heading output will be Unfortunately with larger spacing values there is a...

Страница 5: ...ow 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...

Страница 6: ...he unit Free Mode While in Free Mode the DMS will output data from the sensors without correction by the references For example the Bank Angle data output in Free Mode is calculated directly from the...

Страница 7: ...see below 2 A nine character string representing the Universal Time UTC starting with six digits a decimal point one digit and a space for up to 235959 9 Hours minutes seconds tenth seconds HHMMSS S...

Страница 8: ...or r when the calculated attitude or heading error exceeds the ranges listed above Internal functions that require these error values are disabled while the condition exists The system will continue...

Страница 9: ...nd does not require command mode to be in effect 5 A K or k will clear the Free Mode Command and the Hold Mode Command This command does not require command mode to be in effect 6 An will reinitialize...

Страница 10: ...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 progra...

Страница 11: ...y scale factors can be handled through simple changes in the scale factor stored in the EEPROM in the microprocessor This can be done with a PC and the assistance of the factory Input Logic Commands T...

Страница 12: ...de Longitude 0 6m with DGPS 2 5m without DGPS Environmental Temperature Operating 40 C to 85 C Temperature Storage 55 C to 85 C Vibration Operating 2 5g rms 20 Hz to 2 KHz Vibration Survival 10g rms 2...

Страница 13: ...Watson Industries Inc DMS SGP02 Rev K 03 22 2018 13 Figure2...

Страница 14: ...3 RXD 9 No Connection 20 Forward Acceleration Analog Output 4 Shorted to pin 6 10 Initialization Command 21 Lateral Acceleration Analog Output 5 Signal Ground 11 Velocity Input option 22 Vertical Acce...

Страница 15: ...Watson Industries Inc DMS SGP02 Rev K 03 22 2018 15 Figure 4 GPS Antenna Dimensions...

Страница 16: ...ncluding but not limited to any implied warranty of merchantability or fitness for a particular purpose Excluded from any warranty given by Watson Industries are products that have been subject to abu...

Страница 17: ...elby Street Eau Claire WI 54703 ATTN Service Department Telephone 715 839 0628 Fax 715 839 8248 email support watson gyro com Returning the Product Product shall be packaged making sure there is adequ...

Страница 18: ...Angular Rate ZR 99 9 s 200 s Heading Rate HR 99 9 s 200 s User Channel 1 U1 9 99 VDC 10 VDC User Channel 2 U2 9 99 VDC 10 VDC User Channel 3 U3 9 99 VDC 10 VDC User Channel 4 U4 9 99 VDC 10 VDC Groun...

Страница 19: ...nce Command selected 4 GPS enabled 5 Free Mode selected 6 Logic Input Switches disabled e g Status 040 octal 0 100 000 binary bit 6 is reset No Checksum Error bit 5 is set Ready bit 4 is reset No Velo...

Страница 20: ...keyboard commands Note Most Watson sensors have initialization times that are shorter than 30 seconds Any extra keystrokes other than two spacebars sent during initialization will deactivate command...

Страница 21: ...are two output formats Decimal output _ Command Binary output Command To change the output format 1 Activate Command Mode See above 2 Press the key Command corresponding to the format you want to swi...

Страница 22: ...locity type 2 This is the normal DMS mode non GPS Make sure that the proper analog velocity signal is applied To make this selection the default the next time you power the unit on type in a quote mar...

Страница 23: ...rate type 8 This will bring up the menu 4 Change the baud rate to a new setting To change to 38 400 Baud type 1 To change to 19 200 Baud type 2 To change to 9 600 Baud type 3 To change to 4 800 Baud...

Страница 24: ...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...

Страница 25: ...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...

Страница 26: ...s then shifted left to shift out the 7th bit always set to 1 What remains is a signed fractional word with a resolution of 13 bits plus a sign bit To convert binary data Split each word into two bytes...

Страница 27: ...85 sec 15 015 sec 54 980 sec Example 2 The Unit is seeing these conditions Binary output Format One word per output parameter 7 6 5 4 3 2 1 0 7 6 5 4 3 2 1 0 Data Word MSB LSB Bit 7 of the MSB is set...

Страница 28: ...Convert to units counts scale factor For Bank Elevation Scale factor is 180 32768 counts For Heading Scale factor is 360 65536 counts For Accelerations Scale factor is 10g 32768 counts For Angular Rat...

Страница 29: ...d byte is connected to the lower word These 3 bytes are then shifted left to shift out the 7th bit always set to 1 The MSB is then connected to the 3 lower bytes as a 32 bit long word This long word i...

Страница 30: ...1 bit space a top of high byte Latitude Longitude Altitude Velocity 0x8F 0xF9 0xE7 0xF7 0xDF 0xBD 0x9F 0xF9 0x83 0xBF 0x81 0xA4 Latitude Longitude Altitude Velocity 0x0F 0x79 0x67 0x77 0x5F 0x3D 0x1F...

Страница 31: ...83648 counts 535248752 counts 180 231 counts 44 86403 For Longitude Scale factor is 180 231 or 2147483648 counts 1091240048 counts 180 231 counts 91 46668 For Altitude Scale factor is 32768 feet 216 o...

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