INS100E-A0 Inertial Navigation System
INS100E-A0 Integrated Inertial Navigation System
INS100E-A0-DGI integrated navigation system (hereinafter referred to as integrated navigation system) has built-in high-performance MEMS gyroscope and accelerometer, which can receive internal GNSS data, realize multi-sensor fusion and integrated navigation algorithm, and have short-term inertial navigation capability when GNSS is invalid.
roll & pitch attitude accuracy:0.2°(GNSS valid)
azimuth accuracy:0.5° (1m antenna baseline)
gyro bias stability:4°/h(Allan)
acceleration bias stability:≤0.2mg(Allan)
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DESCRIPTION
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INS100E-A0-DGI integrated navigation system (hereinafter referred to as integrated navigation system) has built-in
high-performance MEMS gyroscope and accelerometer, which can receive internal GNSS data, realize multi-sensor
fusion and integrated navigation algorithm, and have short-term inertial navigation capability when GNSS is invalid.
The product has high reliability and strong environmental adaptability.
FEATURES
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The integrated navigation system can use the satellite navigation information received by the GNSS receiver to carry out integrated
navigation, and output the information of the carrier, such as pitch, roll, course, position, speed, time and the like; 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.
APPLICATION
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●UAV/AUV/Helicopter ●Tactical nuclear weapons ●Aeronautics and astronautics
●Integrated navigation system ●inertial platform stabilizing ●Vehicle navigation
Technical Parameter
INS100E-A0 Integrated Inertial Navigation System
PARAMETER
DIMENSION
Overall dimension of integrated navigation system: 80mm × 53mm × 23mm (length × width × height).
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