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Method for calculating fusion attitude angle based on complementary Kalman filtering algorithm

A Kalman filter and attitude technology, applied in the direction of measuring angles, measuring devices, instruments, etc., can solve problems such as unknown parameter calculation methods

Active Publication Date: 2016-06-08
HUIZHOU FRONT OPTOELECTRONIC TECH CO LTD
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Problems solved by technology

[0004] In order to solve the problem of unknown parameter calculation methods involved in the existing attitude angle fusion algorithm and further improve the accuracy of the attitude angle fusion algorithm, the present invention proposes a method for calculating the fusion attitude angle based on the complementary Kalman filter algorithm, which greatly improves the attitude angle. measurement accuracy

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  • Method for calculating fusion attitude angle based on complementary Kalman filtering algorithm
  • Method for calculating fusion attitude angle based on complementary Kalman filtering algorithm
  • Method for calculating fusion attitude angle based on complementary Kalman filtering algorithm

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Embodiment Construction

[0069] The present invention will be further described below with reference to the accompanying drawings and in combination with preferred embodiments.

[0070] Kalman filtering uses the minimum mean square error as the best criterion for estimation to seek a set of recursive estimation algorithms. The measured value is used to update the estimate of the state variable, and the estimated value at the moment is obtained. The algorithm makes an estimate that meets the minimum mean square error for the signal to be processed according to the established system state equation and measurement equation. Kalman filtering is a powerful method for state vector estimation of state-space models, and it is of great value in theory. Complementary filtering can effectively use each data according to different weights designed. The present invention cleverly combines the Kalman filter algorithm and the complementary filter algorithm, and proposes a method for calculating the fusion attitude...

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Abstract

The invention discloses a method for calculating a fusion attitude angle based on a complementary Kalman filtering algorithm. The method comprises the following steps: building an attitude angle measurement system, calculating and obtaining a first attitude angle according to gyroscope measurement data, calculating and obtaining a second attitude angle according to accelerometer measurement data; fusing the first attitude angle and the second attitude angle according to the Kalman filtering algorithm to obtain a third attitude angle; fusing the first attitude angle, the second attitude angle and the third attitude angle according to a complementary filtering principle to calculate and obtain the fusion attitude angle. According to the method for calculating the fusion attitude angle based on the complementary Kalman filtering algorithm, disclosed by the invention, the measurement precision of the attitude angle is greatly improved.

Description

technical field [0001] The invention relates to the field of attitude angle measurement, in particular to a method for calculating a fusion attitude angle based on a complementary Kalman filter algorithm. Background technique [0002] In the microwave communication anti-shake system, the attitude angle of the microwave antenna is a very important feedback signal. The anti-shake system uses this feedback signal to correct the attitude angle of the microwave antenna, so that the vibration amplitude of the microwave antenna is always within the required accuracy range to ensure The stability of the communication signal. Therefore, the measurement accuracy and stability of microwave antenna attitude angle are very important. Commonly used attitude angle measurement components include gyroscopes, accelerometers, etc. Gyroscopes measure angular velocity signals, but their measured values ​​will drift with time, making the calculated angle values ​​drift with time; accelerometers ...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01C1/00
CPCG01C1/00
Inventor 马建设李国朋苏萍刘彤董瑛
Owner HUIZHOU FRONT OPTOELECTRONIC TECH CO LTD
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