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Accurate Position, Navigation And Timing (master Clock

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Geodetics is an Advanced Sensing and Navigation Company Based in the USA    Accurate Position, Navigation and Timing (Master Clock) in a Single Box Non-ITAR Configurations Tactical Tactical-RTK Advanced ITAR Configurations Tactical RTK-SAASM Advanced SAASM GPS Sensor L1 Standalone L1/L2, RTK-Enabled L1/L2, RTK-Enabled GPS Sensor L1/L2 SAASM, RTK-Enabled L1/L2 SAASM, RTK-Enabled IMU Internal Quartz MEMS Internal Quartz MEMS External FOG IMU Internal Quartz MEMS External FOG or RLG Inertial Navigation System and Master Clock     Configuration (GPS Receiver) DCLS: x3 configurable digital outputs (1PPS, IRIG B002), 3.3V, 50Ω RS232: x1 NMEA ToD message (GPZDA, GPRMC) Frequency: 10 MHz, sine, 0 dBm in 50Ω Network: NTP server (v3, v4) Tactical (L1 only) Tactical-RTK (L1/L2) Tactical-RTK SAASM Advanced (L1/L2) Advanced SAASM  10/100bT LAN interface  Web User Interface (status, configuration, log, SW update)  SNMP Performance Timebase Performance Relative Frequency Variation with Aging 24 hours One month One year Relative Frequency Variation with Temperature (-40°C +85°C) Relative Frequency Variation with Acceleration (any axis) Phase Noise on 10 Mhz Output @10 Hz @100 Hz @1 kHz @100 kHz System Performance Frequency Accuracy Averaged Over 24 hour when Locked on GNSS Phase (1PPS) Drift in Holdover (no reference available) OCXO 5.10-10 _ 5.10 -8 ±5.10-8 -9 Configuration (IMU) CSAC _ 3.10-10 1.10-9 ±5.10-8 ±5.10 /g _ -110dBc/Hz -120dBc/Hz -140dBc/Hz -150dBc/Hz - 70dBc/Hz -113dBc/Hz -128dBc/Hz -140dBc/Hz 3.10-12 1.10-12 4 hours 24 hours 7 days 1.5 μs 30 μs 1 ms 0.2 μs 1.3 μs 30 μs Phase (1 PPS) accuracy to UTC ±50 ns (1δ) ±50 ns (1δ) - Configuration Tactical, Tactical-RTK, Tactical-RTK SAASM Advanced, Advanced SAASM IMU Internal MEMS 1 Internal MEMS 2 External FOG Parameter Range Bias Stability (in-run) Random walk Range Bias Stability (in-run) Random walk Range Bias Stability (in-run) Random walk Accelerometer ±6g Gyroscope ±450°/sec < 0.1 mg 6°/hr 0.04 (m/sec)/√hr ±3g 0.2/√hr ±150°/sec < 0.1 mg 3°/hr 0.04 (m/sec)/√hr ±10g 0.2/√hr ±490°/sec < 0.05 mg 0.05°/hr 0.07 (m/sec)/√hr 0.012/√hr Standalone Mode Horizontal/Vertical Accuracy 1.5 m / 2.5 m Differential Mode Horizontal/Vertical Accuracy - 1.5 m / 2.5 m 0.05 m / 0.1.m 1.0 m / 2.0 m 0.05 m / 0.1 m Standalone Mode Roll-Pitch / Heading Accuracy ±0.2° / ±0.5° Differential Mode Roll-Pitch / Heading Accuracy - Tactical (internal IMU) Tactical-RTK (L1/L2) Tactical-RTK SAASM ±0.2° / ±0.5° ±0.1° / ±0.3° (internal IMU) Advanced (L1/L2) Advanced SAASM ±0.05° / ±0.1° ±0.01° / ±0.05° (external FOG) NOTE: Accuracy must be measured once dynamic alignment is complete * Accuracy is dependent upon GPS satellite system performance, ionospheric conditions, GPS blockage, data link and other factors Configuration (IMU) All Tactical Configurations All Advanced Configurations  Navigation solutions (position, velocity, acceleration, attitude, angular rate, …)  Raw GPS and IMU data (for post processing with Geo-Post)  Full diagnostics Fiber Optic Gyro is standard in Advanced configurations. Built-in support for:  Honeywell HG1900  Honeywell HG1700  Honeywell HG9900  Litton LN200  Other IMU’s on request  Internal safety and monitoring  Systems  Internal BIT with operator notification  Cold Start: 60 s  1 PPS/Time-of-Day: 60 s  Power/status LEDs  Remote/local status, configuration,  event log, software update through web interface Navigation Data Output Rate Up-to 125 Hz Up-to 100 Hz  Temperature in Operation: -40°C to +65°C  Temperature in Storage: -45°C to +85°C  Humidity: 95% RH, non Condensing  Altitude: 35,000 ft  Mechanical (MIL-STD-810G):  Vibration: 7.7 g rms, 20 to 1000 Hz Shock: 20 g, 11 ms  Size: 120 x 100 x 55 mm (4.7” x3.9” x 2.2”) • Weight: 0.75 kg (1.7 lbs.) • Mounting: On a plate, 4 through holes  Input Voltage: 10-30 VDC  Tactical Configurations: 9 W typical, Advanced Configurations: 13 W typical