User manuall v1.1 User manua v1 1

USER MANUAL

UG-301

Bluetooth GPS Navigator

The UG-301 is optimized for good performance and low cost. Its 12 parallel channels and 4000 search bins provide short start-up time and fast signal acquisition. Having fast time-to-first-fix and enhanced acquisition sensitivity of 137dBm and tracking sensitivity of 145dBm provides excellent navigation performance even in urban canyons having limited sky view and under deep foliage, without compromising accuracy. The onboard patch antenna provides good signal reception. In situations where the UG-301 is integrated into an application where the patch antenna has limited view of the sky, external active antenna may be directly connected via the MMCX connector to provide improved signal reception. * Class 2 Bluetooth offers up to 10 meters of wireless operation with Bluetooth-enabled devices such as PDA or Tablet-PC. FEATURES 12 channel GPS receiver Class 2 Bluetooth module 4000 simultaneous time-frequency search bins SBAS (WAAS, EGNOS) support -137dBm acquisition sensitivity -145dBm tracking sensitivity <10 second hot start <45 second cold start 5m CEP accuracy Low power consumption 8hrs operation time
User Manuall v1.1 User Manua v1 1

MECHANICAL DIMENTION

Unit: mm

260.2 500.2

ACCESSORIES
I. Standard: Adaptors (Car & Travel)
II. Optional: External Antenna & PDA Holder
HARDWARE SPECIFICATIONS Item Receiver Type Position Accuracy Time to First Fix Description 12 channel (L1 frequency, C/A code) 5m CEP autonomous 2.0m CEP SBAS <10 sec Hot Start <35 sec Warm Start <45 sec Cold Start <1s -137dBm acquisition -145dBm tracking <4G Altitude < 18,300m Velocity < 514m/se NMEA0183v3.01 Baud rate: 9600 WGS-84 (User definable) 110mA -20oC ~ 60oC MMCX SPP compatible Version 1.1 compliant Class-2 operation 4dBm output level Up to 10m of operation Blue - Bluetooth status Red - Battery low Green - Charging battery Power on/off For BLC-2 type Li-ION (3.6V Rechargeable battery) 5.0V Mini-USB 80mm50mm26mm <180g
Signal Reacquisition Sensitivity Dynamics Operational Limits Protocol Datum Current Consumption Operating Temperature External antenna connector Bluetooth

LED Indicator

Slide Switch Battery DC Input Voltage DC Input Connector Dimension Weight
NMEA OUTPUT MESSAGE SPECIFICATION GGA - GPS FIX DATA Time, position and position-fix related data (number of satellites in use, HDOP, etc.). Format: $GPGGA,<1>,<2>,<3>,<4>,<5>,<6>,<7>,<8>,<9>,M,<10>,M,<11>,<12>,*<13><CR><LF> Example: $GPGGA,104549.04,2447.2038,N,12100.4990,E,1,06,01.7,00078.8,M,0016.3,M,,*5C<CR><LF> Field Example Description 1 104549.04 UTC time in hhmmss.ss format, 000000.00 ~ 235959.2447.2038 Latitude in ddmm.mmmm format Leading zeros transmitted 3 N Latitude hemisphere indicator, N = North, S = South 4 12100.4990 Longitude in dddmm.mmmm format Leading zeros transmitted 5 E Longitude hemisphere indicator, 'E' = East, 'W' = West Position fix quality indicator 0: position fix unavailable 1: valid position fix, SPS mode 2: valid position fix, differential GPS mode Number of satellites in use, 00 ~ 01.7 Horizontal dilution of precision, 00.0 ~ 99.00078.8 Antenna height above/below mean sea level, -9999.9 ~ 17999.0016.3 Geoidal height, -999.9 ~ 9999.Age of DGPS data since last valid RTCM transmission in xxx format (seconds) NULL when DGPS not used 12 Differential reference station ID, 0000 ~ 1023 NULL when DGPS not used 13 5C Checksum Note: The checksum field starts with a * and consists of 2 characters representing a hex number. The checksum is the exclusive OR of all characters between $ and *.
GLL - LATITUDE AND LONGITUDE, WITH TIME OF POSITION FIX AND STATUS Latitude and longitude of current position, time, and status. Format: $GPGLL,<1>,<2>,<3>,<4>,<5>,<6>,<7>*<8><CR><LF> Example: $GPGLL,2447.2073,N,12100.5022,E,104548.04,A,A*65<CR><LF> Field Example Description 1 2447.2073 Latitude in ddmm.mmmm format Leading zeros transmitted 2 N Latitude hemisphere indicator, N = North, S = South 3 12100.5022 Longitude in dddmm.mmmm format Leading zeros transmitted 4 E Longitude hemisphere indicator, 'E' = East, 'W' = West 5 104548.04 UTC time in hhmmss.ss format, 000000.00 ~ 235959.A Status, A = valid position, V = navigation receiver warning 7 A Mode indicator N = Data invalid A = Autonomous D = Differential E = Estimated Checksum GSA - GPS DOP AND ACTIVE SATELLITES GPS receiver operating mode, satellites used for navigation, and DOP values. Format: $GPGSA,<1>,<2>,<3>,<3>,<3>,<3>,<3>,<3>,<3>,<3>,<3>,<3>,<3>,<3>,<4>,<5>,<6>*<7><CR><LF> Example: $GPGSA,A,3,26,21,,,09,17,,,,,,,10.8,02.1,10.6*07<CR><LF> Field Example Description 1 A Mode, M = Manual, A = Automatic Fix type, 1 = not available, 2 = 2D fix, 3 = 3D fix 3 26,21,,,09,17,,,,,, PRN number, 01 to 32, of satellite used in solution, up to 12 transmitted 4 10.8 Position dilution of precision, 00.0 to 99.02.1 Horizontal dilution of precision, 00.0 to 99.10.6 Vertical dilution of precision, 00.0 to 99.07 Checksum

GSV - GPS SATELLITE IN VIEW Number of satellites in view, PRN number, elevation angle, azimuth angle, and C/No. Only up to four satellite details are transmitted per message. Additional satellite in view information is sent in subsequent GSV messages. Format: $GPGSV,<1>,<2>,<3>,<4>,<5>,<6>,<7>,,<4>,<5>,<6>,<7> *<8><CR><LF> Example: $GPGSV,2,1,08,26,50,016,40,09,50,173,39,21,43,316,38,17,41,144,42*7C<CR><LF> $GPGSV,2,2,08,29,38,029,37,10,27,082,32,18,22,309,24,24,09,145,*7B<CR><LF> Field Example Description Total number of GSV messages to be transmitted Number of current GSV message Total number of satellites in view, 00 ~ 26 Satellite PRN number, GPS: 01 ~ 32, SBAS: 33 ~ 64 (33 = PRN120) Satellite elevation number, 00 ~ 90 degrees Satellite azimuth angle, 000 ~ 359 degrees C/No, 00 ~ 99 dB Null when not tracking 8 7C Checksum VTG - COURSE OVER GROUND AND GROUND SPEED Velocity is given as course over ground (COG) and speed over ground (SOG). Format: GPVTG,<1>,T,<2>,M,<3>,N,<4>,K,<5>*<6><CR><LF> Example: $GPVTG,221.0,T,224.3,M,016.0,N,0029.6,K,A*1F<CR><LF> Field Example Description 1 221.0 True course over ground, 000.0 ~ 359.9 degrees 2 224.3 Magnetic course over ground, 000.0 ~ 359.9 degrees 3 016.0 Speed over ground, 000.0 ~ 999.9 knots 4 0029.6 Speed over ground, 0000.0 ~ 1800.0 kilometers per hour 5 A Mode indicator N = Data invalid A = Autonomous D = Differential E = Estimated 6 1F Checksum
RMC - RECOMMANDED MINIMUM SPECIFIC GPS/TRANSIT DATA Time, date, position, course and speed data. Format: $GPRMC,<1>,<2>,<3>,<4>,<5>,<6>,<7>,<8>,<9>,<10>,<11>,<12>*<13><CR><LF> Example: $GPRMC,104549.04,A,2447.2038,N,12100.4990,E,016.0,221.0,250304,003.3,W,A*22<CR><LF> Field Example Description 1 104549.04 UTC time in hhmmss.ss format, 000000.00 ~ 235959.A Status, V = navigation receiver warning, A = valid position 3 2447.2038 Latitude in dddmm.mmmm format Leading zeros transmitted 4 N Latitude hemisphere indicator, N = North, S = South 5 12100.4990 Longitude in dddmm.mmmm format Leading zeros transmitted 6 E Longitude hemisphere indicator, 'E' = East, 'W' = West 7 016.0 Speed over ground, 000.0 ~ 999.9 knots 8 221.0 Course over ground, 000.0 ~ 359.9 degrees UTC date of position fix, ddmmyy format 10 003.3 Magnetic variation, 000.0 ~ 180.0 degrees 11 W Magnetic variation direction, E = East, W = West 12 A Mode indicator N = Data invalid A = Autonomous D = Differential E = Estimated Checksum ZDA TIME AND DATE Format: $GPZDA,<1>,<2>,<3>,<4>,<5>,<6>*<7><CR><LF> Example: $GPZDA, 104548.04,25,03,2004,,*6C<CR><LF> Field Example Description 1 104548.04 UTC time in hhmmss.ss format, 000000.00 ~ 235959.25 UTC time: day (01. 31) UTC time: month (01. 12) UTC time: year (4 digit year) 5 Local zone hour Not being output by the receiver (NULL) 6 Local zone minutes Not being output by the receiver (NULL) 7 6C Checksum

Tactical Advanced Land Inertial Navigator (TALIN )
CONTINUOUS POSITION, POINTING, AND TARGETING SOLUTIONS
The continued evolution of the proven, best-value navigation system for the digital battlefield
Flexible, reliable, best-value INS/GPS navigator

System Characteristics

State-of-the-art plugNplay sensors to facilitate technology upgrades & platform missionizations Instant on! On-the-move alignment Multiple accuracy configurations to meet different applications requirements

Operating Ranges

Attitude: Alignment and orientation in any direction Angular Rate: +200 deg/sec MTBF: >25,000 hours

Power Requirements

18-32 Vdc: <30 watts*

System Features

Flexible tactical configurations for combat vehicles, target acquisition, main battle tanks, infantry fighting vehicles, mortar systems, and artillery systems
In use on over 30 platforms, including Bradley FIST, Stryker, Bradley A3, Mortar Fire Control System, NLOS, IBCT FIST, IBCT Mortar, USMC CLAWS, Towed Artillery Digitization and Swiss FO
TALIN 3000 TALIN 4000 TALIN 5000

Thermal Operating Range

No cooling required: -46C to 71C (-51F to 160F)

Navigation Sensors

Standard: 3-axis inertial sensors (internal), VMS, DAGR, PLGR
Performance Horizontal Pos INU only INU/VMS INU/VMS/GPS PPS INU/VMS/GPS SPS Vertical Pos INU only INU/VMS INU/VMS/GPS PPS INU/VMS/GPS SPS Heading/Pointing Accuracy (RMS) *Sec (Lat) Heading Stability (RMS) Pitch & Roll Accuracy (RMS) Max Alignment Time Static or Gyro Compass Dynamic or On the Move

TALIN 2000

Software
< 35m CEP 0.5% of DT CEP < 10m CEP < 60m CEP < 25m CEP 0.35% of DT CEP < 10m CEP < 60m CEP < 18m CEP < 12m CEP 0.25% of DT CEP 0.20% of DT CEP < 10m CEP < 10m CEP < 60m CEP < 60m CEP
Modular partitioned for cost-effective system missionization

Weight

<16 pounds (<7kg)
< 30m PE 0.25% of DT PE < 10m PE < 75m PE < 4.0 mils or < 2.0 mils*
< 16 m PE 0.20% of DT PE < 10m PE < 75m PE < 2.0 mils or < 1.0 mils*
< 10 m PE 0.15% of DT PE < 10m PE < 75m PE < 1.0 mils or < 0.5 mils*
< 7m PE 0.10% of DT PE < 10m PE < 75m PE < 0.7 mils or < 0.35 mils*

Interfaces

Standard: 1553A & B/RS-422/RS-232 serial host interface Optional: Additional RS-422/RS-232 data interface, turret encoderes, laser range finders

Form Factor

< 0.4 mils/hr < 0.3 mils/hr < 0.2 mils/hr < 0.15 mils/hr
Approx. 5.1h x 7.0w x 8.5l inches (excluding flanges & connectors)

< 1.0 mils

< 0.5 mils

< 0.35 mils

Installation
Can be hard mounted in any orientation
< 5.0 minutes < 12.0 minutes
< 10.0 minutes < 16.0 minutes

< 15.0 minutes

*Application and configuration dependent

< 16.0 minutes

Values shown are per definitions in TALIN system specifications
Honeywell Aerospace 1944 E. Sky Harbor Circle Phoenix, AZ 85034 Domestic: 1.800.601.3099 International: 1.602.365.3099 www.honeywell.com
N61-0610-000-000 February Honeywell International Inc.