Inertial Measurement System DMS-SGP02 Two Antenna GPS
The DMS-SGP02 is equipped with a dual antenna GPS system, so it provides a GPS heading reference signal even while the unit is stationary.
Features:
- Solid State, Strapdown System
- GPS Heading Reference
- Latitude, Longitude, Altitude Output
- Low Cost
- Rugged, High Reliability
- Vibration Resistant
- Analog and RS-232 Serial Outputs
- One Year Limited Warranty
- Engineering Support
Description
The DMS-SGP02 is a miniaturized version of the DMS-EGP02. To allow for a smaller package, the DMS-SGP02 uses our S series MEMS rate gyro.
The DMS may be used in almost any application where triaxial angular rate and acceleration data is required. This inertial sensor provides both angular rate and acceleration outputs in analog and digital formats. The DMS features six accelerometer outputs. The X, Y, and Z axis outputs represent the accelerations in the plane of the vehicle body, while the second set of three outputs measure the acceleration aligned with an earth-level coordinate system. This allows forward and lateral acceleration measurements that are essentially free of gravity influences. The triaxial sensor set allows software alignment of sensors, greatly reducing any alignment errors. The serial interface is highly configurable and provides access to almost all operational parameters.
The DMS-SGP02 is designed for vehicle applications where accurate heading is required, but a magnetic compass is infeasible. This sensor is equipped with a dual GPS antenna system that provides heading data even when the vehicle is not is motion. The addition of the GPS antennas also gives vehicle velocity data to the DMS which enhances the unit’s performance during highly dynamic maneuvers such as sharp turns. This makes the DMS-SGP02 inertial gyro sensor a more complete system since it does not require velocity information to be supplied from an external sensor.
The DMS-SGP02 is useful in automotive testing, vehicle dynamics, and marine applications. This sensor can be used as a replacement for the discontinued Watson IMU-E604, and is most useful in applications where strong magnetic fields make heading data from a fluxgate magnetometer unreliable.
Specifications
Attitude |
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Range: Bank | ±180° | ||
Range: Elevation | ±90° | ||
Resolution: | 0.02° | Binary mode (14 bit) | |
Analog Scale Factor: | 18°/V | ±10V Bank ±5V Elevation |
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Accuracy: Static | ±0.5° | ||
* | Accuracy: Dynamic | 2% | |
GPS Heading |
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Range: | 0° – 360° | ||
Resolution: | 0.02° | Binary mode (14 bit) | |
Analog Scale Factor: | 18°/V | ±10V Output | |
Accuracy: Static | 0.5° | Based on antenna spacing. See figure 1 | |
* | Accuracy: Dynamic or Relative | 2% | ±0.1°/sec (without GPS) |
Angular Rate |
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Range: Roll, Pitch, Yaw | ±100°/sec | ||
Resolution: | 0.025°/sec | Binary mode (14 bit) | |
Analog Scale Factor: | 10°/sec/V | ±10V Output | |
Scale Factor Accuracy: | 2% | ||
Bias: Roll, Pitch, Yaw | < 0.3°/sec | ||
Non-Linearity: | < 0.05% | Full scale range | |
Bandwidth: | 20 Hz | ||
Acceleration |
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Range: X, Y, Z | ±10g | ||
Range: Forward, Lateral, Vertical | ±10g | ||
Resolution: | 4mg | ||
Analog Scale Factor: | 1g/V | ±10V Output | |
Scale Factor Accuracy: | 1% | ||
Bias: X, Y, Z | < 10mg | ||
Non-Linearity: | 0.1% | Full scale range | |
Bandwidth: | 3 Hz | ||
GPS Positioning |
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Range: Latitude | ±90° | ||
Range: Longitude | ±180° | ||
Range: Altitude | 0ft to 21500ft | ||
Resolution: Latitude, Longitude | 0.0000013° | Binary mode (28 bit) | |
Resolution: Altitude | 2 ft | Settable: Above mean sea level or GPS Geodetic Corrected | |
Accuracy: Latitude, Longitude | ±0.6m (with DGPS) | ±2.5m (without DGPS) | |
Environmental |
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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 | 20 Hz to 2 KHz | |
Shock: Survival | 500g | 10mS ½ sine wave | |
Electrical |
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Frame Rate: | 71.1 Hz | Maximum | |
Startup Time: Data | 5 sec | ||
† | Startup Time: Satellite acquisition | 5 min | Typical |
Input Power: | 10 to 35VDC | 4.9W | |
Input Current: | 410mA @ 12VDC | 205mA @ 24VDC | |
Input Velocity: (Optional) | ±10VDC | Full scale (±400kph) | |
Digital Output: | RS-232 | ||
Analog Output: | ±10VDC | ||
Analog Output Impedance: | 300 Ohm | Per line | |
Physical |
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Axis Alignment: | < 0.25° | ||
Size: Including Mounting Flanges | 3.24″W x 5.78″L x 3.50″H | 8.2 x 14.7 x 8.9 (cm) | |
Weight: | 31 oz (1.9 lb) | 879 grams (0.9 Kg) | |
Connection: RS-232 | 9 pin female “D” subminiature | ||
Connection: Power / Analog Outputs | 25 pin male “D” subminiature | ||
Connection: Antenna (Qty 2) | SMA | Antenna cable length: 3.0m | |
* | Using velocity data with GPS mode on. Actual accuracy can be calculated as the listed percentage multiplied by the change in value over the entire dynamic maneuver. |
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† | Acquisition time for GPS units is typical for the contiguous United States. Acquisition time may differ due to interference in your geographic area. | ||
• | Specifications are subject to change without notice. | ||
• | This product may be subject to export restrictions. Export Classification ECCN 7A994. |
Applications
- Aerospace
- Stabilized Camera
- Flight Testing
- Attitude Indicator
- UAV Control/Display
- Compass Systems
- Drone: Primary Gyro
- UAV: Research
- Unmanned Vehicles
- Backup Attitude Instrument
- Heading Reference
- Land
- Skid Pad Testing
- Road Surface Measurement
- Tractor Control
- Unmanned Vehicles
- Camera Stabilization
- Tractor Navigation Control
- Heading Reference
- Ocean
- Satellite Tracking Antenna
- Surface Navigation
- Barge Instrumentation