Starts from the Best Quality

Inertial Navigation System (INS) is a type of navigation system that uses sensors to measure the linear and angular acceleration of an object. It works by constantly updating the position and orientation of the object based on these measurements. INS is self-contained and does not rely on external references such as GPS signals or landmarks, making it suitable for use in environments where these references are unavailable or unreliable. INS is commonly used in aircraft, missiles, and spacecraft to provide navigation and guidance information. It is also used in some ground vehicles and marine vessels. One of the main advantages of INS is its high accuracy and stability, as it is not affected by external factors such as atmospheric conditions or interference.


INS2000 Inertial Navigation System

– High Stability, High Reliability, High Accuracy

– High Survivability, Fully Calibrated INS

– Provide Accurately Real-time 3D Position, Speed, Acceleration, Attitude Angle, Angular Rate, etc.

– Position Accuracy (Pure Inertial Navigation):100m (100s)

– Attitude Angle Error: 2°

– Overload Resistance:10000g, IP67 Protection

– Wide Temperature: -40°C~+85°C


INS1000 Inertial Navigation System

– Real-time Measure Accurately the Attitude Angle,Position, Speed, Acceleration and Angular Rate

for High Speed Self-spinning Flying Body

– Angular Range: ±150°/s, ±400°/s (optional)

– Acceleration Range:±10g, ±100g (optional)

– Attitude Angle Error: 2°, Anti-rotation: 30r/s

– High Stability, High Reliability, High Survivability in Harsh Environment

– Overload Resistance: 10000g