HG5700 Inertial Measurement Unit
The HG5700 is a product that bridges the performance gap between the HG1700 high performance tactical-grade IMU and the HG9900 high performance navigation-grade IMU. The HG5700 fulfills the need for better performance than the HG1700 at a smaller size and lower cost than the HG9900.
The HG5700’s three Ring Laser Gyroscopes (RLG), three vibrating beam accelerometers (VBA) and associated electronics are all environmentally sealed in rugged aluminum housing. The HG5700 also employs an external environmental ring isolator to filter unwanted sensor inputs commonly encountered in real world applications.
The HG5700 simplifies system integration by offering many configurable features – such as data rate output and flight control filtering. External heat sinks and cooling are not required by HG5700, facilitating greater flexibility in systems design and integration.
The IMU capabilities include up to 3600Hz output, inertial and flight control outputs, internal or external sync, and customizable filters and data output. The INS capabilities include initialization/ transfer align, north finding/ keeping, multiple aiding source input, flight control and navigation output, and is PVT, LOS, and UTC capable." "The HG5700 is designed and built at a Honeywell facility in the USA. It typically has an ECCN of 7A003.d.1 but can vary depending on model selected. It generally requires an export license.
Specifications
Performance
Accel Bias In-Run Stability (mg 1σ)
- 0.035
Key Benefits
- All inertial sensors utilized in our tactical IMUs are designed, developed, and manufactured by Honeywell
- Drop-in replacement for the HG1700 IMU for enhanced performance
- Industry standard RS-422 serial interface
- RLG design is based on the highly successful navigation grade GG1320 technology
- Units feature a wide range of factory configurable interface protocols including Synchronous Data Link Control (SDLC), Asynchronous serial (UART), and Gated Clock
Gyro sensor technology
- Ring Laser
Gyro Operating Range
- 1074°/sec to 1620°/sec
Gyro Bias Repeatability
- 0.05 °∕hr 1σ
Gyro Bias In-Run Stability
- 0.015 °∕hr 1σ
Gyro ARW
- 0.008
Accelerometer Sensor Technology
- Quartz
Accelerometer Operating Range
- 37 (up to 70)
Accel Bias Repeatability (mg 1σ)
- 0.2
Accel Velocity Random Walk (VRW)
- 0.02
Physical
Weight
- 1360 g
Dimensions
- 102 H x 92 D (127 ring diameter)
Power and Electrical
Supply Voltage
- +5V, +15V
Power Consumption
- <10W Watt
Mechanical
Operating Temperature
- -54°C to +85°C
Connectivity and Systems
Data Rate
- 600 (flight control) and 100 (inertial), up to 3600
Communication Protocols
- SDLC, ASYNC, UART, Gated Clock
Communication Ports
- RS422 & discrete 5V logic