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Nanjing Sky MEMS Technology Co.,Ltd.
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Inertial Navigation Vertical Reference Gyro Sensor For Precision Agriculture VG500

Nanjing Sky MEMS Technology Co.,Ltd.
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Nanjing Sky MEMS Technology Co.,Ltd.
City: Nanjing
Province/State: Jiangsu
Country/Region: China
Tel: +86-25-83356968
Contact Person:
Mr David zhu

Inertial Navigation Vertical Reference Gyro Sensor For Precision Agriculture VG500

Brand Name : SkyMEMS
Model Number : VG500
Certification : CE, FCC, ROHS
Place of Origin : Nanjing, Jiangsu
MOQ : 1PCS
Price : discuss personally
Payment Terms : Western Union, MoneyGram, L/C, T/T, D/A, D/P
Supply Ability : 1000PCS for month
Delivery Time : 3-5 days after payment
Packaging Details : Strong cartn with PET strap for VG500 Vertical Reference Gyro
High Performance Vertical Reference Gyro : Yes
Pitch Accuracy : 0.3°
Roll Accuracy : 0.3°
Resolution : 0.01°
Power supply : 9-35V
Current : 40mA
Working Temperature : -40℃~+85℃
Factory Calibrated : Yes
Shock Resistance : 3000g
Ruggedized Enclosure : IP67
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Inertial Navigation Vertical Reference Gyro System Sensor for Precision Agriculture VG500


Product Description

VG500 Vertical Reference Gyro is an intelligent vertical gyro for measuring roll and pitch angles in dynamic environments. VG500 calculates stabilized roll and pitch angles by integrating the angular rate sensor outputs. The adaptive vertical erection algorithm is used to compensate for gyro bias-induced errors based on a long term gravity reference provided by the accelerometers.

VG500 measures acceleration and rotation rate about three orthogonal axes. VG500 employs on-board digital processing to provide a factory calibrated unit with internal compensation for

deterministic error sources. It is widely used in the applications include UAV flight control, avionics, and platform stabilization.


Main Features

- High Performance Vertical Gyro, dynamic/static measurement

- High Reliability MEMS Sensors

- Enhanced Kalman Filter Algorithm

- Ultra Low Gyro Noise

- Fully Temperature Compensated

- Wide Sensor Bandwidth

- Bandwidth Filtering Capability

- IP67 protection

- Pitch accuracy 0.3°, Roll accuracy 0.3°, resolution: 0.01°

- Small size: L104 × W55 × H26 mm(custom service supported)


Typical Application

VG500 Vertical Reference Gyro delivers a high performance cost-effective solution that meets the demanding environmental requirements for operation in control, navigation and stabilization systems, it has been widely applied in the following solutions, such as:

• UAV Flight Control

• Platform Stabilization

• Avionics

• Automotive Testing

• Unmanned Vehicle Control


Technical Specifications


Technical Specs
Attitude parametersPitch accuracy0.3°
Roll accuracy0.3°
Resolution0.01°
Tilt marginPitch ± 90º, roll ± 180º
Physical propertiesDimensionL103.8 x W55.4 x H26 (mm)
Weight150 g
RS-232/RS485 interface connectoroptional
Interface characteristicsStart-up delay<50 ms
Maximum sampling rate50 times/s[2]
Serial port communication rate2400~115200 baud rate
Digital output formatBinary high performance protocol
Power supplyVoltage9-35V
Current (max)60mA
Operation mode40mA
EnvironmentStore range-55℃~+100℃
Operation temperature-40℃~+85℃
Shock resistance2000g

Competitive Advantages

High Performance Vertical Reference Gyro

- Advanced MEMS Sensors

- Enhanced Kalman Filter Algorithm

- Fully Temperature Compensated

- High MTBF

- Environmentally sealed (IP67), compact design

- High shock resistance

- Full tests and individual calibration from -40 to 85°C

- High cost effective


FAQ

What is Disadvantages of INS?

• Mean‐squared navigation errors increase with time.

• Cost, including:

– Acquisition cost, which can be an order of magnitude (or more) higher than GPS receivers.

– Operations cost, including the crew actions and time required for initializing position and attitude. Time required for initializing INS attitude by gyrocompass alignment is measured in minutes. TTFF for GPS receivers is measured in seconds.

– Maintenance cost. Electromechanical avionics systems (e.g., INS) tend to have higher failure rates and repair cost than purely electronic avionics systems (e.g., GPS).

• Size and weight, which have been shrinking

• Power requirements, which have been shrinking along with size and weight but are still higher than those for GPS receivers.

• Heat dissipation, which is proportional to and shrinking with power requirements.


Product Tags:

vertical reference sensor

      

inertial reference unit

      
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