INS200A-E Inertial Navigation System

DESCRIPTION

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INS200A-E integrated navigation system has built-in high-performance MEMS gyroscope and accelerometer, 

which can receive external GNSS data, realize multi-sensor fusion and integrated navigation algorithm, 

and has short-term inertial navigation capability when GNSS is invalid.

FEATURES

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The integrated navigation system can use the satellite navigation information received from the outside to carry out 

integrated navigation, and output the pitch, roll, course, position, speed, time and other information of the carrier; 

After losing the signal, it outputs the position, velocity and attitude information of inertial solution, and has a certain 

navigation accuracy maintenance function in a short time. When combined with navigation, it can output the raw 

information that can be used for post-processing to be processed by the IE post-processing software of NovAtel.

APPLICATION

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●UAV/AUV/Helicopter     ●Tactical nuclear weapons    ●Aeronautics and astronautics

●Integrated navigation system     ●inertial platform stabilizing   ●Vehicle navigation