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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
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High Overload Resistance Inertial Navigation Module , Military Navigation Systems For Rocket

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

High Overload Resistance Inertial Navigation Module , Military Navigation Systems For Rocket

Brand Name : SkyMEMS
Model Number : INS100
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 INS100 serial MEMS Gyro
High Performance Inertial Navigation System : Yes
Accelerometer Range : ±10g
Gyro Dynamic Range : ±150°/s, ±400°/s (support custom design)
Attitude Angle Error : ≤2°
Anti-rotation : 30r/s
Overload Resistance : 10000g
Input Current : ≤300mA
Output Data : 8 bit parallel data output
Operating Temperature : -40~85°C
Factory Calibrated : Yes
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Miniature High Overload Resistance INS sensor Inertial Navigation System for Rocket INS100


Product Description

INS100 Inertial Navigation System adopts multiple technologies including MEMS, ASIC, micro system integration design, and advanced navigation calculating technologies, it can be used to measure attitude angle, position, speed, acceleration, angular speed, etc. for high speed aerocraft such as rocket, the system enjoys high reliability, high stability, and adjustment in harsh environment.

The system enjoys the advantages such as small size, light weight, low cost, low power consumption, quck startup, high reliability, excellent adjustment in dynamic environment, it has been widely applied in tactical weapon, rocket measurement fields.


Main Features

Real-time measure accurately the attitude angle, position, speed, acceleration and angular rate for high speed self-spinning flying body

Acceleration range:±10g, ±100g, angular range: ±150°/s, ±400°/s

Attitude angle error: 2°, anti-rotation: 30r/s

High stability, high reliability, high survivability in harsh environment, overload resistance: 10000g

Wide temperature: -40°C~+85°C


Typical Application

INS100 Inertial Navigation System is a strap-down 6-axis Inertial Navigation System, it is composed of 3 linear accelerometers and 3 linear angular rate sensors (gyros), it can measures the complete motion. INS100 has been widely applied in the special solutions, such as:

- Mid-sized & large UAV

- Avionics

- Gyro-stabilized camera

- Flight data recorder

- Unmanned Ground Vehicle

- Camera and 3D scanner

- SATCOM antenna

- Machine Control

- Weapon


Technical Specifications

Technical Specs
Measurement Rangeacceleration:±10g, angular rate: ±150°/s,±400°/s (support custom design)
Attitude angle error≤2°
Anti-rotation30r/s
Overload resistance10000g
Power supplyvoltage: V=5±0.25V, current I≤300mA
Output data8 bit parallel data output
Weight≤5kg
DimensionФ120*250mm
working temperature-40~85°C

Competitive Advantages

High Performance INS Inertial Navigation System

- Highly accurate, reliable and temperature stable

- Advanced, extendable, embedded Kalman Filter based sensor fusion algorithms

- State-of-the-art algorithms for different dynamic motions of Vessels, Ships, Helicopters, UAV, UUV, UGV, AGV, ROV, Gimbals and Land Vehicles

- Full temperature calibration of all sensing elements.

- Environmentally sealed (IP67), compact design

- Proven and robust filter design

- Overload resistance: 10,000g

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

- High cost effective


FAQ

What is Inertial Navigation System (INS)?

Inertial navigation is a self-contained navigation technique in which measurements provided by accelerometers and gyroscopes are used to track the position and orientation of an object relative to a known starting point, orientation and velocity. Inertial measurement units (IMUs) typically contain three orthogonal rate-gyroscopes and three orthogonal accelerometers, measuring angular velocity and linear acceleration respectively. By processing signals from these devices it is possible to track the position and orientation of a device.


Product Tags:

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ins navigation system

      
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