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A dual accelerometer calibration method without a turntable

An accelerometer and dual-acceleration technology, applied in the field of inertial navigation and positioning, can solve the problems of restricting wide application and harsh use conditions, and achieve the effect of getting rid of dependence and accurate calibration

Active Publication Date: 2020-09-25
湖南湘科浩宇科技有限公司
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Problems solved by technology

However, the use conditions of this method are relatively harsh. First, a turntable with a certain accuracy is required as a reference to ensure that the relative conversion relationship between multiple positions is known. Time data sampling; these two conditions of use (especially the need for a turntable with a certain accuracy) greatly limit the wide application of this method in engineering

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  • A dual accelerometer calibration method without a turntable
  • A dual accelerometer calibration method without a turntable
  • A dual accelerometer calibration method without a turntable

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Embodiment Construction

[0063] A dual-accelerometer calibration method under the condition of no turntable is to perform online error calibration on the accelerometer in the carrier inertial navigation system. There are at least two accelerometers in the carrier inertial navigation system, which are called accelerometer 1 and accelerometer 1 respectively. Measure 2, first place the carrier inertial navigation system in a static state;

[0064] Under the condition of using a turntable, the calibration of the accelerometer is realized.

[0065] The core idea of ​​this calibration scheme is to require the inertial navigation system to be in a static state as a whole, and use the three-axis output of the accelerometer 1 (defined as: f 1 ) to calculate the pitch angle and roll angle of the inertial navigation system in the current state, and assuming that the heading angle of the current inertial navigation system is 0 degrees, the attitude transformation matrix (defined as: C 1 ), the attitude transfor...

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Abstract

The invention discloses a turntable-free double-accelerometer calibration method. At least two accelerometers are arranged in a carrier inertial navigation system, and are respectively called an accelerometer A and an accelerometer B; and the carrier inertial navigation system is made to be in a stationary state. The method include the following steps that: the zero offset error calibration modelsof the accelerometer A and accelerometer B are constructed and defined, and at the same time, error measurement vectors in the error calibration models are obtained; and the Kalman filtering method is adopted to filter the zero offset error calibration models of the accelerometer A and accelerometer B, and with the error observation vectors adopted as filtering input, the tri-axial output zero offset error calibration values of the accelerometer A and the accelerometer B at a k time point are obtained during the convergence processing of filtering. According to the method of the present invention, on the basis of the speed error of the inertial navigation system, the Kalman filtering technology is adopted to realize the accurate online estimation of the zero offset of the accelerometers.

Description

technical field [0001] The invention relates to the field of inertial navigation and positioning, in particular to a dual accelerometer calibration method without a turntable, and is an accelerometer calibration method suitable for loading two or more accelerometer platforms without a turntable. Background technique [0002] Inertial technology is a general term for inertial guidance, inertial navigation and inertial measurement technology, and its theoretical basis is based on the laws of classical mechanics. Among them, inertial navigation is such a technology, the speed can be obtained by integrating the output of the accelerometer once, the position change can be obtained by integrating twice, and the direction and magnitude of the rotation can be determined by the measured value of the gyroscope. Through the combined use of gyroscopes and accelerometers, the position of the vehicle can be determined. Inertial navigation only needs to obtain the precise initial position...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01C21/16G01P21/00
Inventor 梁源徐兵
Owner 湖南湘科浩宇科技有限公司