Applications range from PNT for stationary or slowly moving platforms such as Aerostats to PNT for high-dynamic aircraft and everything in between. AEVEX’s proven Assured PNT products are designed to provide critical PNT information under demanding conditions.
GEODETICS PRODUCTS
ASSURED-PNT FOR LAND, AIR AND SEA PROVEN. EXPANSIVE. UNIQUE.
www.geodetics.com
GEODETICS PRODUCTS
ADVANCING MISSION SUCCESS We take a long-term, strategic view of our client relationships to establish a depth and breadth of mission understanding. Our agility and expertise allow us to rapidly identify, develop, and deliver tailored solutions to meet any design, engineering, modi fi cation, testing, operations, sustainment, and analysis requirement.
ABOUT US AEVEX Aerospace supports defense and commercial clients worldwide by providing full-spectrum aviation, remote sensing, and analysis solutions. Our areas of expertise include custom design and engineering, sensor integration and sustainment, aircraft modi fi cation, test and certi fi cation, mission operations services, advanced intelligence data processing, exploitation, and dissemination solutions. Tailored hardware and software mission system tools from AEVEX also include assured precision navigation systems. AEVEX uses agile and customized approaches to rapidly de fi ne, develop, and deliver specialized solutions for airborne special mission needs for the U.S. government, partner nations, and commercial businesses.
Headquartered in Solana Beach, California.
AEVEX has major offices in: California, Massachusetts, New Mexico, North Carolina, Ohio, and Virginia.
years of Experience over 20
With over 20 years of experience, Geodetics products are the go-to for Assured Positioning, Navigation and Timing (A-PNT) systems and sensor fusion for mobile applications in the air, on land and at sea. As a US-based company, we are proud to offer products that comply with military-grade SAASM and M-Code GPS requirements. All elements of Geodetics’ products including underlying algorithms, electrical, mechanical and software components are designed, tested, manufactured, and maintained in-house by our dedicated teams of project managers, scientists, algorithm developers and software, hardware, testing, and support engineers.
TEAM
Innovators, technical experts and partners focused on developing customized solutions for clients with mission-critical challenges.
SPECIALITIES
Assured Positioning, Navigation and Timing (A-PNT) systems and advanced sensor fusion technologies. LiDAR and multi-modal imaging solutions for mobile and UAV (drone) applications.
CORE COMPETENCIES
Advanced algorithms, Kalman fi ltering, data and sensor fusion/integration and National Security measures offering cost-ef fi cient solutions tailored to support our clients’ unique and evolving applications.
CAPABILITIES
Relative navigation, integrated timing systems, high-speed positioning for manned and autonomous vehicles in aerospace and Defense programs as well as state-of-the-art LiDAR and multi-modal imaging solutions for mobile and UAV (drone) operations in both domestic and international markets
Geo-APNT™
Available with SAASM or Commercial GPS Receivers PTP Grandmaster (IEEE 1588 v2) NTP server (v3, v4) Upgradable to TCX O, OCXO or Rubidium oscillator Precise 1 PPS, 10 MHz and other timing signals Support for MEMS, FOG, RLG, and Navigation grade IMU’s Support for RTK and PPK
Assured Position, Navigation and Timing (Master Clock) in a Single Box
Geo-APNT Applications
Airborne
HIGH-ACCURACY NAVIGATION SYSTEM
Observation payload
•
Radar
Optronics Electronic warfare Flying test bench Flight analysis Tactical UAV navigation
Proven performance in wide range of application areas • Proven performance in wide range of application areas • Available with SAASM or Commercial GPS • Centimeter-level position accuracy (RMS) with RTK and PPK • In-motion dynamic alignment • Support for low, medium and high-dynamic platforms • GPS/IMU Post-processing support with Geodetics’ RTD-Post Geo-APNT offers a fully integrated GPS-aided inertial navigation solution supporting a wide range of IMU grades and provides a high-performance trusted positioning and navigation capability.
• • •
Ground • • • • Sensor support Anti IED jamming systems Mobile radios and C3I Robotics
HIGH-PERFORMANCE TIME SERVER
Geo-APNT maintains an accurate internal timescale with very low power consumption via a low-phase noise OCXO (other oscillator options available upon request). Precise time and frequency signals are available as 1 PPS, unmodulated IRIG B timecode, 10 MHz, and NMEA time-of-day messages. • PTP grandmaster (IEEE 1588 v2) • Network: NTP server (v3, v4) • DCLS: digital outputs (1PPS, IRIG B002, PPO, ALARM), 3.3V, 50 Ω • RS232: x1 NMEA ToD message (GPZDA, GPRMC) • Frequency: 10 MHz, sine, 0 dBm in 50 Ω
Sensor support Radar, Sonar Optronics Electronic warfare Communications
•
• •
networks Offshore / DSO platforms
•
Geo-APNT™ Assured Positioning, Navigation and Timing
Posion Accuracy* Con fi gura on (GPS Receiver)
Monitoring
Technical Specifications Data Recording / Logging • Navigation solutions (position, velocity, acceleration, attitude, angular rate, …) • Raw GPS and IMU data (for post processing with RTD-Post) • Full diagnostics External IMU Support Fiber Optic Gyro is standard in Advanced con fi gurations. Built-in support for: • Honeywell HG1900, HG1700, HG9900 • Litton LN200 • Other IMU’s available upon request
Di ff eren al Mode Horizontal/Ver cal Accuracy (RMS)
Standalone Mode Horizontal/Ver cal Accuracy (RMS)
• Power/status LEDs • Remote/local status, con fi guration, • event log, software update through web interface Environmental • 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 Physical • 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
Tac cal (L1 only) Tac cal-RTK (L1/L2) Tac cal-RTK SAASM Advanced (L1/L2) Advanced SAASM
1.5 m / 2.5 m 1.5 m / 2.5 m
-
0.05 m / 0.1.m
1.0 m / 2.0 m
0.05 m / 0.1 m
Dynamic Attitude Accuracy* Con fi gura on (IMU)
Standalone Mode Roll-Pitch / Heading Accuracy (RMS)
Di ff eren al Mode Roll-Pitch / Heading Accuracy (RMS)
Tac cal (internal IMU) Tac cal-RTK Tac cal-RTK SAASM (internal IMU)
±0.2° / ±0.5°
-
Safety and Diagnostics • Internal safety and monitoring • Systems Operational Readiness • Cold Start: 60 s (commercial) • 1 PPS/Time-of-Day: 60 s Power • Input Voltage: 10-30 VDC
±0.2° / ±0.5°
±0.1° / ±0.3°
Advanced Advanced SAASM (external FOG)
±0.05° / ±0.1°
±0.01° / ±0.05°
NOTE: Accuracy must be measured once dynamic alignment is complete * Accuracy is dependent upon GPS satellite system performance, ionospheric condions, GPS blockage, environmental condins, data link and other factors
• Tactical Con fi gurations: 9 W typical, Advanced Con fi gurations: 13 W typical
Geo-APNT IMU Performance (Internal)
Con fi g.
IMU
Parameter
Accelerometer
Gyros
Range
±3g
±150°/sec
Timing Output Signals • PTP grandmaster (IEEE 1588 v2) • Network: NTP server (v3, v4) • DCLS: con fi gurable digital outputs (1PPS, IRIG B002, PPO, ALARM), 3.3V, 50 Ω • RS232: x1 NMEA ToD message (GPZDA, GPRMC) • Frequency: 10 MHz, sine, 0 dBm in 50 Ω
Bias Stability (in-run) Random walk Bias Stability (in-run) Random walk Range Bias Stability (in-run) Random walk Range
< 0.1 mg
3°/hr.
MEMS 1
0.04 (m/sec)/ √ hr.
0. 2/√ hr. ±200°/sec
±3g
Tactical, Tactical-RTK, Tactical-RTK SAASM
MEMS 2
< 0.1 mg
2.2°/hr.
0.04 (m/sec)/ √ hr.
0.09/ √ hr. ±450°/sec
Management
±4g , ±10g < 0.05 mg
MEMS High- Performance
• 10/100bT LAN interface • Web User Interface (status, con fi guration, log, SW update) • SNMP
0.8°/hr.
0.02 (m/sec)/ √ hr.
0.06/ √ hr.
Time and Frequency Performance Performance
Oscillator Level I
Oscillator Level II
Geo-APNT IMU Performance (External)*
Time-base Performance
24 hours / One year
24 hours / One year 0.5x10 -12 /0.5x10 -10
Con fi gura on
IMU
Parameter
Accelerometer
Gyroscope ±490°/sec
Range
±10g
Rela ve Frequency Varia on with Aging (based on 30-day aging) Rela ve Frequency Varia on with Temperature (-40°C +75°C) Phase Noise on 10 Mhz. Output @10 Hz @100 Hz @1 kHz Other oscillators available upon request
Fiber Op c Gyro Ring Laser Gyro
Advanced, Advanced SAASM Advanced, Advanced SAASM
1x10 -12 /1x10 -10 ±5x10 -11
Bias Stability (in-run) Random walk Bias Stability (in-run) Random walk Range
< 7.5 mg
1°/hr.
0.07 (m/sec)/ √ hr.
0.012/ √ hr. ±1074°/sec
±2x10 -11
±37g
-120dBc/Hz -140dBc/Hz -145dBc/Hz
-120dBc/Hz -145dBc/Hz -150dBc/Hz
< 1 mg
1°/hr.
0.001 (m/sec)/ √ hr.
0.125/ √ hr.
* Built-in Support for Honeywell HG1900, HG1700, HG9900, Litton LN200. Other IMU’s available upon request.
Civilian GPS
Internal data logging
Geo-iNAV ® Support for wide range of IMU’s MEMS (internal) Tactical (external) Navigation (external)
SAASM GPS
Path to M-CODE
High Performance Inertial Navigation System
KEY FEATURES • Centimeter-level position accuracy (dual-frequency RTK con fi guration) • GPS Processing with Precise Instantaneous Network positioning based on Geodetics’ Epoch - by - Epoch® technology • In-motion dynamic alignment • Support for low, medium and high dynamic platforms • Post-processing support with RTDPost • Mil-Spec ruggedization
GEO-INAV ® is a fully-integrated gps-aided inertial navigation system supporting a wide range of IMU grades and providing a high performance, trusted positioning and navigation capability Geo-iNAV ® is offered in several con fi gurations designed to meet a wide range of requirements, and is available for both commercial and military applications: • Geo-iNAV ® Commercial: Designed for civilian navigation applications (no ITAR restrictions) • Geo-iNAV ® SAASM: Designed for applications that have a military SAASM GPS requirement
APPLICATIONS
UAV and UGV navigation and control
Military and defense security
Robotic and ROV control
Oil and gas exploration
Transportation safety and maintenance
Mobile mapping systems and photogrammetry
Construction and structural management
Geo-iNAV ® High Performance Inertial Navigation System
Typical Posi on, Velocity, Accelera on, A tude Accuracy (RMS)
1
GPS Op ons
Processing Op ons
Posi on (Horizontal/Ver cal)
Roll, Pitch / Heading (Tac cal MEMS, Advanced IMU) ±0.2° / ±0.5° , ±0.05° / ±0.1° ±0.1° / ±0.3° , ±0.01° / ±0.05° ±0.2° / ±0.5° , ±0.05° / ±0.1°
Velocity, Accelera on
Standalone Mode L1/L2 RTK Mode Standalone Mode L1/L2 RTK Mode
1.5 m / 2.5 m 0.05 m / 0.1 m 1.0 m / 2.0 m 0.05 m / 0.1 m
0.1 m/s, 0.15 m/s 2 0.02 m/s, 0.1 m/s 2 0.1 m/s, 0.15 m/s 2 0.02 m/s, 0.1 m/s 2
Commercial
SAASM
±0.1° / ±0.3° , ±0.01° / ±0.05° 1 Accuracy is dependent on GPS satellite system performance, ionospheric condi ons, GPS blockage, environmental condi ns , data link and other factors.
IMU Speci fi ca ons
\
Parameter
MEMS*
Fiber Op c Gyro
Ring Laser Gyro (ITAR)
Gyroscope Dynamic Range
±100°/sec or ±200°/sec
±490°/sec.
±1074°/sec.
Gyroscope Bias In-Run Stability (1 σ ) Gyroscope Angle Random Walk (1 σ ) Accelerometer Dynamic Range Accelerometer Bias In-Run Stability (1 σ ) Accelerometer Velocity Random Walk (1 σ )
2.2°/hr.
2°/hr.
1°/hr.
0.09°/ √ hr.
0.012°/ √ hr.
0.125°/ √ hr.
±3g
±10g
±37g 1mg
0.1mg
7.5mg
0.04(m/sec)/ √ hr.
0.07(m/sec)/ √ hr.
0.001(m/sec)/ √ hr.
[ [
*: For more MEMS, FOG, or RLG IMU op ons please contact us
Technical Speci fic a ons
Parameter Parameter
Commercial Con fi gura ons
SAASM Con fi gura ons
External power connector TNC GPS antenna connector 1 Ethernet data port and 3 RS-232 serial ports
External power connector TNC GPS antenna connector 1 Ethernet data port 3 RS-232 serial ports, 1PPS output 4 status LED
Interfaces
1PPS output 4 status LEDs SAASM Keyload Connector SAASM Zeroize bu on.
GPS Frequency Tracking Key Loading Size / Weight / Power Temperature Range Real-Time Data Output Data Recording/Logging
L1/L2
L1 & L2 (P/Y Code)
N/A DS-101 33.8 in 3 (4.73x3.95x1.81) / 20 oz. / 10 – 30 VDC @ 2 Amps min. (not including external IMU’s) Speci fi ed: -20°C to +65°C Opera ng: -40°C to +70°C Naviga on solu ons at 125 Hz (MEMS), 100 Hz. (FOG, RLG). available via Ethernet, RS-232 Naviga on solu ons,raw GPS & IMU data (for post-processing with RTD-Post)
Relative Navigation Systems Geo-RelNAV™
A unique GPS / IMU based navigation system
The relative navigation information computed by Geo-RelNAV includes relative position, relative velocity (closure rate), and relative orientation.
KEY FEATURES
• Minimized sensor size and weight to meet payload restrictions • Available with SAASM and commercial GPS receivers • Available with different grades of IMU’s to support a wide range of application requirements • Real Time Kinematic GPS & Relative Extended Kalman Filter • On-Board data logging of all sensor raw and navigation solution data • The relative navigation can be provided between one leader and multiple followers • The system can be upgraded to vision-aided navigation for operations in GPS-denied conditions. Please contact us for more details
Probe & Drogue
Boom & Recepticle
APPLICATIONS
• Aerial refueling • Shipboard landing
• Approach and auto-landing • Autonomous driving vehicles • Sense & Avoid for commercial UAVs • Autonomous landing for UAVs • Autonomous platooning (V2V-Vehicle to Vehicle) • UxV Collision Avoidance and Swarming • UxV Leader/Follower Applications • Sports action following
Shipboard Landing: Runway
Shipboard Landing: Landing Deck
Relative Navigation Systems Geo-RelNAV™
RELATIVE NAVIGATION A CCURACY
RELATIVE POSITION
CEP 50%; σ H<0.15m
σV<0.45m
CEP 95%; σ H<0.50m CEP 99%; σ H<1.0m
σ V<0.30m
σ V<0.15m
Landing Point
HORIZONTAL POSITION
VERTICAL POSITION
*Accuracy is dependent on GPS satellite performance, ionospheric conditions, satellite visibility, environmental conditions, datalink, platform separation and other factors CEP 50%; Đ H<0.15m
The system can be upgraded to vision-aided navigation for operations in GPS-denied conditions. Please contact us for more details.
TECHNICAL SPECIFICATIONS ( SINGLE BOX)
Paramer Size / Weight / Power (w/o IMU) Environmental Temperature Range Interfaces
Commercial Con fi gurations 33.5 in3 (3.95 x 3.05 x 2.06) / 14.4 oz / 10 - 30 VDC @ 2 Amps min. MIL - 810E, MIL -461 Compliant Speci fi ed : 20O C to + 65O C l Operating : -40O C to 70O C External power connector, TNC GPS antenna connectors, 1 Ethernet data port, 3 RS-232 serial ports, 1PPS output, 4 status LEDs. Navigation solutions at up-to 125 Hz. available via Ethernet or RS-232 Relative navigation solutions, absolute navigation solutions, raw GPS, IMU
Real-Time Data Output Data Recording / Logging
Hybrid Dual-GPS/INS Navigation System Geo-hNAV ®
Dual - GPS / INS navigation
Easy integration “Small footprint and low power consumption”
Geo-hNAV con fi gurations can be customized to satisfy the most demanding inertial navigation accurac and performance requirements be customized to satisfy the most demanding inertial navigation accuracy and performance requirements
Provides accurate orientation for static or slowly moving
Available in Civilian or SAASM
Flexibility
Geo-hNAV™ is a ruggedized, fully-integrated hybrid dual-GPS-aided inertial navigation system which delivers consistent position and attitude measurement accuracy whether the platform is static or moving. Geo-hNAV™ is offered in several con fi gurations designed to meet a wide range of navigation application requirements. Con fi gurations are available for both commercial and military applications:
• Multiple IMU con fi gurations available with internal MEMS or external FOG/RLG IMUs • Multiple GPS con fi gurations available with both civilian and SAASM receivers
High Navigation Performances
Centimeter level positioning (RMS) with dualfrequency RTK con fi guration
•
Geo-hNAV Commercial Designed for civilian navigation applications (no ITAR restrictions)
0.05° heading measurement accuracy (RMS) both in low and high dynamic conditions (for 3 m GPS baseline separation)
•
Geo-hNAV SAASM Designed for navigation applications that have a military SAASM GPS requirement
Easy to Integrate into Your System
• SWaP, BIT with log • Several types of data interface: RS-232 and Ethernet
APPLICATIONS
Geo-pointing for onboard sensors for low dynamic platforms such as aerostats, boats, tanks Camera, EO/IR sensor stabilization Antenna pointing Weaponry pointing Vehicle testing in static and mobile conditions Hovering UAS platforms
•
High Dynamic Antenna-Camera
Low Dynamic Camera -LiDAR
Static Camera -LiDAR
•
• • •
•
Static Antenna
Mortar
Weapon
Hybrid Dual-GPS/INS Navigation System Geo-hNAV ®
Geo-hNAV Con fi gura ons Non-ITAR Con fi gura ons
GPS Sensor
IMU
Tac cal
L1/L2, RTK-Enabled L1/L2, RTK-Enabled
Internal Quartz MEMS
Advanced
External FOG
ITAR Con fi gura ons Tac cal SAASM Advanced SAASM
GPS Sensor
IMU
L1/L2 SAASM, RTK-Enabled L1/L2 SAASM, RTK-Enabled
Internal Quartz MEMS
External FOG or RLG (other IMU’s available upon request)
Output Rates Through Serial or RS232 Interface Con fi gura on (IMU) Naviga on Data Output Rate All Tac cal Con fi gura ons Up-to 125 Hz All Advanced Con fi gura ons Up-to 100 Hz Technical Speci fi ca ons Power • Input Voltage: 10-30 VDC • Civilian:
IMU Performance
Environmental • Civilian Opera ng Temperature: -40°C to +65°C (-40°F to 150°F) • SAASM Opera ng Temperature: -40°C to +70°C (-40°F to 158°F) • Storage: -55°C to +85°C (-67°F to +185°F) • Humidity: 95% RH, non-Condensing • Vibra ns and Shock: MIL-STD 810G, 514.5 and 516.5 • EMC/EMI: MIL-STD 461 Geo-hNAV Enclosure • Size: 120 x 100 x 55 mm (4.7” x3.9” x 2”.2) • Weight: 0.75 kg (1.7 lbs.) • Moun ng: On a plate, 4 through holes Interfaces • External power connector • Dual TNC GPS antenna connector • 1 Ethernet data port • 3 RS232 serial ports • 1 PPS output • IMU connector for external IMU • 4 status LEDs SAASM Con fi gur ns • SAASM Keyload connectors (DS- 101) • SAASM Zeroize bu ons
• Internal IMU: 8 W typical • External IMU: 15 to 20 W typical (external IMU powered by main unit) • SAASM: • Internal IMU: 10 W typical • External IMU: 10 to 13 W typical (external IMU powered by main unit) Data Recording / Logging • Naviga n solu ns (posi n, velocity, accelera n, a tude, angular rate, …) • Raw GPS and IMU data (for post processing with RTD-Post) • Full diagnos cs External IMU Support Fiber Op c Gyro is standard in Advanced con fi gura ns. Built-in support for:
Posi on Accuracy*
• Honeywell HG1900 • Honeywell HG1700 • Honeywell HG9900 • Li on LN200 • Other IMU’ s on request
Safety and Diagnos cs • Internal safety and monitoring systems • Internal BIT with operator no fi ca on
NOTE: Accuracy must be measured once dynamic alignment is complete *Accuracy is dependent upon GPS satellite system performance, ionospheric condi ons, GPS blockage, environmental condi ns, data link and other factors. **The GPS-based heading accuracy and baseline length have approximately linear rela onship
PROVEN. EXPANSIVE. UNIQUE.
GEODETICS PRODUCTS
2649 Ariane Drive San Diego, CA 92117 (858) 729-0872 geodetics@aevex.com www.geodetics.com
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