Because of the manufacturing process, the data measured by the inertial sensor usually has a certain error.The first error is the offset error, which is…
The gyro theodolite consists of a gyroscope, a theodolite and a tripod. (1) gyroscope The gyroscope is the core of the system, which is mainly composed of…
The AHRS, called the Attitude Reference System, consists of multiple axial sensors that provide the aircraft with heading, roll and roll information. Such…
1 zero deviation and zero drift Zero offset is the output of the gyroscope when the input angular velocity is zero (that is, the gyroscope is at rest). It…
This type of receiver is mainly used for the navigation of moving carrier. It can give the position and speed of the carrier in real time.This kind of…
Latitude error or damping error Cause: the vertical damping method is used. Elimination method: (1) External compensation method -- calculate the size and…
Optical fiber gyro north finder can work reliably in the full weather, and is not affected by the external environment such as the earth's magnetic field,…
Fiber-optic gyroscope uses two beams from the laser to be injected into the same optical fiber, but in opposite directions, the beam resisting rotation…
The cheapest and most widely used MEMS gyroscopes use as few analog circuits as possible, and few digital ones.The output impedance of these gyroscopes is…
AHRS, commonly known as heading reference system, can provide accurate and reliable roll, pitch, heading and other attitude and navigation information for…
The main disadvantage of using IMU navigation is that they usually accumulate errors, including Abbe errors. Because the guidance system will continue to…
The earliest known gyroscope-like device was invented in 1817 by John Bohnenberger of Germany. At first he called this device "machine", based on a sphere…
The inertial measurement unit is composed of three accelerometers and three gyroscopes. The three accelerometers and gyroscopes are designed to measure…
The main technologies that need to be broken through in fiber optic gyroscopes are the instability of the scale factor caused by the loss of sensitivity…
Gyrocompass difference refers to the error caused by bai technical problems in gyrocompass, and du is often affected by latitude zhi degree and speed, but…