Sign In | Join Free | My peerflix.com
peerflix.com
Nanjing Sky MEMS Technology Co.,Ltd.
Focus on MEMS Inertial Measurement Technologies and Products Aerospace Level Quality, Reliable Selection AHRS Inclinometer Fiber Optic Gyro IMU INS GNSS/INS MEMS Acc MEMS Gyro E-compass VG MRU Shock
Home > Vertical Reference Gyro >

High Performance Vertical Reference Gyro Aircraft Wide Sensor Bandwidth

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

High Performance Vertical Reference Gyro Aircraft Wide Sensor Bandwidth

Brand Name : SkyMEMS
Model Number : VG300
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 VG300 Vertical Reference Gyro
Enhanced MEMS sensing technology : Yes
Pitch Accuracy : 0.5°
Roll Accuracy : 0.5°
Resolution : 0.1°
Tilt Range : Pitch ± 90º, roll ± 180º
Start-up Delay : <50 ms
Sampling Rate : 50 times/s
Factory Calibrated : Yes
Shock Resistance : 3000g
Ruggedized Enclosure : IP67
Contact Now

Mems Gyroscope High Performance Aircraft Gyro Vertical Reference Gyro Sensor VG300


Product Description

VG300 Vertical Reference Gyro is a robust entry-level

Vertical Gyro System that utilizes MEMS-based inertial sensors and Extended Kalman Filter algorithms to provide unmatched value in terms of both price and performance. The VG300 is a next generation replacement used in dynamic control and land navigation systems with over 1000 systems currently in service.

This rugged low-cost inertial system meets the demanding environmental requirements for operation in a wide variety of land

vehicle and marine platform systems, and it is ideally suited for cost sensitive high-volume OEM applications.


Main Features

- High Performance Vertical Gyro, dynamic/static measurement

- High Reliability MEMS Sensors

- Enhanced Kalman Filter Algorithm

- Wide Temp Range (-40°C to +85°C)

- Ultra Low Gyro Noise

- Fully Temperature Compensated

- Light Weight 260 grams

- Small Size

- Wide Sensor Bandwidth

- Bandwidth Filtering Capability

- IP67 protection

- Pitch accuracy 0.5°, Roll accuracy 0.5°, resolution: 0.1°

- Nonlinear compensation, perpendicular compensation

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


Typical Application

VG300 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

• EO/IR Stabilization

• Antenna Stabilization & Pointing

• Railway Motion Monitoring

• Flight Control

• Navigation

• Automotive Testing

• Unmanned Vehicle Control


Technical Specifications

Technical Specs
Attitude parameterspitch accuracy0.5° [1]
Roll accuracy0.5° [1]
Resolution0.1°
Tilt marginPitch ± 90º, roll ± 180º
Physical propertiesDimensionL104 × W55 × H26 mm
Weight260 g
RS-232/RS485 interface connector10 pins
Interface characteristicsStart-up delay<50 ms
Maximum sampling rate50 times/s[2]
Serial port communication rate2400~19200 baud rate
Digital output formatBinary high performance protocol
Power supplyVoltageDC +5V or 11-35V
Current (max)40mA
Operation mode30mA
EnvironmentStore range-40℃~+125℃
Operation temperature-40℃~+85℃
Shock resistance3000g

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 does an INS consist of??

• An inertial navigation uses gyroscopes and accelerometers to maintain an estimate of the position, velocity, and attitude rates of

the vehicle in or on which the INS is carried, which could be a land

vehicle, aircraft, spacecraft, missile, surface ship, or submarine.

• An INS consists of the following:

– An IMU

– Instrument support electronics

– Navigation computers (one or more) calculate the gravitational

acceleration (not measured by accelerometers) and doubly integrate the net acceleration to maintain an estimate of the position of the host vehicle.


Product Tags:

vertical reference sensor

      

inertial reference unit

      
China Customized Inflatable Bumper Ball Game Bubble Adult Grass CE supplier

High Performance Vertical Reference Gyro Aircraft Wide Sensor Bandwidth Images

Inquiry Cart 0
Send your message to this supplier
 
From:
Enter your email please.
To: Nanjing Sky MEMS Technology Co.,Ltd.
Subject:
Message:
Characters Remaining: (0/3000)