A method for diagnosing faults of UAV gyroscopes

A diagnosis method and technology of a fault diagnosis device, which can be applied to instruments, measuring devices, etc., can solve the problems of hyperplane bias of optimal classification decision function, failure to discuss the influence of fault diagnosis accuracy, and reduction of fault diagnosis accuracy, so as to improve the fault diagnosis accuracy. Diagnostic accuracy, rich digital signal processing, and miniaturization

Active Publication Date: 2021-05-25
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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Problems solved by technology

However, this method does not discuss the influence of sample data set imbalance and noise singularity on the accuracy of fault diagnosis.
During the training process of support vector machine, the imbalance of positive and negative sample data sets and noise interference will lead to the hyperplane bias of the optimal classification decision function and reduce the accuracy of fault diagnosis

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  • A method for diagnosing faults of UAV gyroscopes
  • A method for diagnosing faults of UAV gyroscopes
  • A method for diagnosing faults of UAV gyroscopes

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Embodiment Construction

[0048] A method for diagnosing a UAV gyroscope fault proposed by the present invention will be described in detail below in conjunction with the accompanying drawings. For the fault diagnosis device used in the diagnosis method of the present invention, the fault diagnosis device based on the TMS320F28335 platform is taken as an example, but it is not limited to the TMS320F28335 platform.

[0049] Such as figure 1 and 2 As shown, the fault diagnosis device includes a TMS320F28335 digital signal processor, a clock circuit, a power supply circuit, a reset circuit, a serial port level conversion circuit, an analog conversion circuit, and a memory expansion circuit. It is characterized by:

[0050] The TMS320F28335 digital signal processor is TI's C2000 series TMS320F28335 chip, with a main frequency of 150MHz; 32-bit single-precision hardware floating-point unit and 32×32-bit hardware multiplication unit; 16-channel 0-3.3-volt 12 1-bit A / D conversion module, single-channel max...

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Abstract

The invention discloses a fault diagnosis method for a UAV gyroscope. Based on the fuzzy technology, the degree of proximity between the sample and the expected value is calculated, and the probability of the degree of proximity is used to design the sample membership factor, and the membership factor is configured to indicate support In the mathematical model of the vector machine, the influence of sample distribution imbalance and noise characteristics is eliminated. Support vector machine training is carried out offline, and the decision function parameters of the optimal interval classification surface for distinguishing positive and negative samples are obtained. When the drone is flying, the attitude signal output by the airborne sensor gyroscope is collected in real time, and the db4 wavelet basis decomposition method is used to extract it. The eigenvector of the signal is normalized, and then input to the decision function of the optimal interval classification surface to calculate the category label of the signal to be divided in real time and identify the fault condition of the gyroscope. The diagnosis method of the invention significantly reduces the bias degree of the fault classification hyperplane, improves the fault diagnosis accuracy, has a small calculation amount, and realizes the online real-time performance of the fault diagnosis algorithm.

Description

technical field [0001] The invention relates to a fault diagnosis of a sensor, in particular to a fault diagnosis method for a gyroscope of an unmanned aerial vehicle. Background technique [0002] With the advantages of UAV 3D (Dull: boring, Dirty: harsh environment, Dangerous: dangerous) mission execution advantages and low price advantages, UAVs are widely used in military reconnaissance, target positioning, electronic warfare, missile interception, etc. and civilian fields such as emergency rescue and disaster relief, inspection of power lines and oil and gas pipelines, anti-terrorism and stability maintenance, and aerial photography. [0003] UAV platforms in the field of military applications are often equipped with multi-type jamming equipment such as TACAN and radar; The navigation signal, the radiation signal generated by the engine operation, and the complex airborne electromagnetic environment produce uncertain interference on the output signal of the gyroscope, ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01C25/00
CPCG01C25/005
Inventor 罗秋凤周国兴陈喆吴武斌
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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