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A North-finding Method with Single Gyro in Arbitrary Four Positions

A four-position, gyro technology, applied in the inertial field, can solve problems such as fixed phase difference or symmetrical positions, and achieve the effects of convenient operation, reduced conditional constraints, and strong practicability

Active Publication Date: 2021-11-02
CENT SOUTH UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The present invention provides a single gyro north-finding method with any four positions, which not only solves the problem that the traditional four-position scheme must have a fixed phase difference or symmetrical positions for data measurement due to the reduction of the constraints of the rotation position and the number of sensitive elements, but also has the advantages of convenient and reliable operation. With strong characteristics, it can be widely used in the accurate orientation of weapon systems such as military missiles and artillery, mine engineering and penetration measurement that require accurate azimuth references and other fields

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  • A North-finding Method with Single Gyro in Arbitrary Four Positions
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  • A North-finding Method with Single Gyro in Arbitrary Four Positions

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Embodiment

[0034] An arbitrary four-position single gyro north-seeking method, which specifically includes the following steps, see details for details figure 1 :

[0035] The first step is to install the inertial device. The inertial device includes a gyroscope and an accelerometer. Here, only one gyroscope and one accelerometer are needed, and the sensitive shafts of the gyroscope and accelerometer are installed in the same direction, and the motor drives the shaft to rotate; figure 2 The space coordinates formed by X, Y, and Z are indicated in the figure, O is the origin of the coordinates, and the gyroscope and accelerometer are installed on the X axis.

[0036] Step 2: After receiving the north-seeking command, the motor is locked at the current position P1, and stays for a period of time (according to the requirements of the working conditions and accuracy, 100 seconds is selected here), and the initial value of the gyroscope and accelerometer in the inertial device is obtained. ...

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Abstract

The invention discloses an arbitrary four-position single gyro north-seeking method, comprising the following steps: installing an inertial device; obtaining static data of the gyroscope and accelerometer in the inertial device at the initial position; synchronously rotating the gyroscope and the accelerometer at a certain angle to obtain the inertial device The static data of the device at this position; the gyroscope and the accelerometer continue to rotate synchronously to a certain angle to obtain the static data of the inertial device at this position; the gyroscope and the accelerometer rotate again synchronously to a certain angle to obtain the static data of the inertial device at this position; The azimuth angle is obtained by substituting the above-obtained mean value of the gyro output and the mean value of the accelerometer output into the unique azimuth angle solving formula. By applying the method of the present invention, the effect is: the present invention can solve the problem that the traditional four-position scheme must have a fixed phase difference or a symmetrical position for data measurement due to the constraints of reducing the rotational position and the number of sensitive elements; the present invention has the advantages of convenient operation and strong reliability. characteristics and a wide range of applications.

Description

technical field [0001] The invention relates to the field of inertial technology, in particular to an arbitrary four-position single gyro north-seeking method. Background technique [0002] Gyro North Finder is a high-precision inertial instrument that can automatically indicate azimuth in all weather under static conditions, and has broad application prospects in military and civilian sectors. [0003] The main function of the gyro north finder is to provide attitude and azimuth reference for the carrier. Most of the current north finders use fiber optic gyroscope and accelerometer as the main sensitive components to achieve north finding. [0004] In the prior art, there are two-position, four-position, multi-position and continuous rotation methods for north-seeking schemes based on indexing. These traditional methods have the following defects: some north-seeking methods require fixed position measurement, such as the traditional four-position rotational orthogonality. ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01C17/00G01C21/18
CPCG01C17/00G01C21/18
Inventor 芦佳振赵雪松郭昱良于振华韩松来
Owner CENT SOUTH UNIV