CN113029202A - Redundancy strapdown inertial measurement unit fault detection method based on parameter optimization depth confidence model - Google Patents
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Abstract
The invention discloses a redundant strapdown inertial measurement unit fault detection method based on a parameter optimization depth confidence model, belonging to the field of aircraft navigation, guidance and control and comprising the following steps of: s1, acquiring output data of the redundant strapdown inertial measurement unit, and constructing a training set and a test set based on the output data; s2, training the deep confidence model by adopting a training set to obtain a trained deep confidence model; s3, optimizing the structural parameters of the trained depth confidence model to obtain a depth confidence model with optimal structural parameters; s4, inputting the test set into a depth confidence model with the optimal structural parameters, and performing redundant strapdown inertial measurement unit fault detection; the invention solves the problems of inaccurate fault modeling, difficult manual feature extraction and limitation on manual parameter adjustment in the conventional redundant strapdown inertial measurement unit fault detection method.
Description
Technical Field
The invention belongs to the field of aircraft navigation, guidance and control, and particularly relates to a redundant strapdown inertial measurement unit fault detection method based on a parameter optimization depth confidence model.
Background
In many important aerospace applications, reliability requirements for aircraft navigation systems are very high. The adoption of the redundant strapdown inertial measurement unit can significantly improve the reliability of the navigation system, provided that the redundant strapdown inertial measurement unit has a high fault tolerance, which can be realized by using a Fault Detection and Isolation (FDI) technology.
In recent years, deep learning has been pursued by more and more researchers due to its excellent classification ability. Under the condition that a system model is unknown, features can be extracted through deep learning model training data, and classification is achieved. The Deep Belief Network (DBN) has good feature learning and classification capabilities as a deep network model, and is widely applied to various fields. At present, the deep confidence network structure is mostly determined by experience or by manually adjusting parameters, and the development of the deep confidence network structure is limited to a certain extent.
Disclosure of Invention
Aiming at the defects in the prior art, the redundancy strapdown inertial measurement unit fault detection method based on the parameter optimization depth confidence model solves the problems that the fault modeling is inaccurate, the characteristics are difficult to extract manually and the manual parameter adjustment is limited in the conventional redundancy strapdown inertial measurement unit fault detection method.
In order to achieve the purpose of the invention, the invention adopts the technical scheme that: a redundant strapdown inertial measurement unit fault detection method based on a parameter optimization depth confidence model comprises the following steps:
s1, acquiring output data of the redundant strapdown inertial measurement unit, and constructing a training set and a test set based on the output data;
s2, training the deep confidence model by adopting a training set to obtain a trained deep confidence model;
s3, optimizing the structural parameters of the trained depth confidence model to obtain a depth confidence model with optimal structural parameters;
and S4, inputting the test set into the depth confidence model with the optimal structural parameters, and detecting the fault of the redundant strapdown inertial measurement unit.
Further, the depth confidence model in step S2 is composed of multiple layers of limiting boltzmann machine units, and the depth confidence model specifically includes a layer 1 limiting boltzmann machine unit, a layer 2 limiting boltzmann machine unit, a layer 3 limiting boltzmann machine unit, a layer 4 limiting boltzmann machine unit, and up to an nth layer limiting boltzmann machine unit, which are connected in sequence.
Further, the step S2 includes the following sub-steps:
s21, training the limiting Boltzmann machine units layer by layer to obtain all the limiting Boltzmann machine units after training;
s22, extracting features of the data output by the trained nth layer limiting Boltzmann machine unit to obtain an output result;
s23, comparing the output result with the actual value to obtain an error value;
and S24, distributing error values from the trained layer 1 limiting Boltzmann machine unit to the trained layer n limiting Boltzmann machine unit in sequence by adopting a back propagation method for parameter fine adjustment, and obtaining the trained deep confidence model.
The beneficial effects of the above further scheme are: the method can automatically extract and learn the characteristics of the data, and overcomes the difficulty of manually extracting the characteristics.
Further, the step S21 includes the following steps:
s211, initializing an iteration parameter r, wherein r = 1;
s212, inputting the training set into the 1 st layer of limiting Boltzmann machine unit, training the 1 st layer of limiting Boltzmann machine unit, updating the weight and the bias of the r layer of limiting Boltzmann machine unit, and obtaining the trained r layer of limiting Boltzmann machine unit;
s213, adding 1 to r, judging whether r is equal to n +1, if yes, finishing the training of all the limiting Boltzmann machine units, and if not, jumping to the step S212.
The beneficial effects of the above further scheme are: the training efficiency is improved, and the problem of local optimization is improved.
Further, the step S3 includes the following sub-steps:
s31, initializing an iteration parameter k, wherein k = 0, and taking the trained depth confidence model as a current optimized depth confidence model;
s32, calculating the fitness of the current optimized depth confidence model;
s33, judging whether the fitness meets a set threshold, if so, taking the current optimized depth confidence model as the depth confidence model with the optimal structural parameters, ending the substeps, if not, adding 1 to k, and jumping to the step S34;
s34, calculating the position and the speed of the structural parameter by adopting the parameter updating model, and carrying out the optimization of the kth iteration on the structural parameter of the current optimized depth confidence model based on the position and the speed of the structural parameter to obtain a kth suboptimal depth confidence model;
s35, taking the k-th sub-optimal depth confidence model as the current optimal depth confidence model, and jumping to the step S32.
The beneficial effects of the above further scheme are: the method can overcome the randomness of manually selecting parameters, reasonably determines the network structure parameters, and is favorable for improving the performance of fault detection of the redundant strapdown inertial measurement unit.
Further, the formula for calculating the fitness of the current optimized depth confidence model in step S32 is as follows:
wherein,fin order to be a degree of fitness,Mfor the total number of verifications of the current optimized deep confidence model,mis as followsmThe result of the secondary verification is that,bin order to correctly classify the number of samples,cthe number of misclassified samples.
Further, in step S34, the parameter update model is:
wherein,αin order to be the inertial weight,β 1is a first one of the acceleration factors, and,β 2is the second one of the acceleration factors, and,v ij k is as followskStructural parameters of sub-iterationiTo (1) ajThe speed of the dimensional variable is then determined,v ij k+1is as followsk+Structural parameters of 1 iterationiTo (1) ajThe speed of the dimensional variable is then determined,x ij k is as followskStructural parameters of sub-iterationiTo (1) ajThe position of the dimension-variable is,x ij k+1is as followsk+Structural parameters of 1 iterationiTo (1) ajThe position of the dimension-variable is,p ij k is as followskStructural parameters of sub-iterationiTo (1) ajThe optimal position of the individual extrema of the dimensional variable,r j k is as followskThe first of the sub-iterationsjThe global optimum position of the dimensional variable,a 1、a 2is a random number between 0 and 1.
The beneficial effects of the above further scheme are: the method can avoid the situation that the parameters fall into the local optimal solution, and obtain the globally optimal parameters.
In conclusion, the beneficial effects of the invention are as follows: the method adopts the parameter optimization depth confidence model to extract the fault characteristics of the redundant strapdown inertial measurement unit, overcomes the problems of inaccurate fault modeling, difficult manual characteristic extraction, difficult parameter selection and the like of the conventional method, realizes the fault detection of the redundant strapdown inertial measurement unit, and is beneficial to improving the reliability of an aircraft navigation system.
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FIG. 1 is a flow chart of a redundant strapdown inertial measurement unit fault detection method based on a parameter optimized depth confidence model;
FIG. 2 is a block diagram of a depth confidence model;
FIG. 3 is a schematic diagram of a configuration of a regular dodecahedron redundant strapdown inertial mount.
Detailed Description
The following description of the embodiments of the present invention is provided to facilitate the understanding of the present invention by those skilled in the art, but it should be understood that the present invention is not limited to the scope of the embodiments, and it will be apparent to those skilled in the art that various changes may be made without departing from the spirit and scope of the invention as defined and defined in the appended claims, and all matters produced by the invention using the inventive concept are protected.
As shown in fig. 1, a redundant strapdown inertial measurement unit fault detection method based on a parameter optimization depth confidence model includes the following steps:
s1, acquiring output data of the redundant strapdown inertial measurement unit, and constructing a training set and a test set based on the output data;
after the output data of the redundant strapdown inertial measurement unit is collected, the fault type of the redundant strapdown inertial measurement unit needs to be marked, and then a training set and a test set are constructed according to the fault type of the redundant strapdown inertial measurement unit.
S2, training the deep confidence model by adopting a training set to obtain a trained deep confidence model;
in step S2, the depth confidence model is composed of multiple layers of limiting boltzmann machine units, and the depth confidence model specifically includes a layer 1 limiting boltzmann machine unit, a layer 2 limiting boltzmann machine unit, a layer 3 limiting boltzmann machine unit, a layer 4 limiting boltzmann machine unit, and up to an nth limiting boltzmann machine unit, which are connected in sequence, as shown in fig. 2.
Step S2 includes the following substeps:
s21, training the limiting Boltzmann machine units layer by layer to obtain all the limiting Boltzmann machine units after training;
step S21 includes the following steps:
s211, initializing an iteration parameter r, wherein r = 1;
s212, inputting the training set into the 1 st layer of limiting Boltzmann machine unit, training the 1 st layer of limiting Boltzmann machine unit, updating the weight and the bias of the r layer of limiting Boltzmann machine unit, and obtaining the trained r layer of limiting Boltzmann machine unit;
s213, adding 1 to r, judging whether r is equal to n +1, if yes, finishing the training of all the limiting Boltzmann machine units, and if not, jumping to the step S212.
S22, extracting features of the data output by the trained nth layer limiting Boltzmann machine unit to obtain an output result;
s23, comparing the output result with the actual value to obtain an error value;
and S24, distributing error values from the trained layer 1 limiting Boltzmann machine unit to the trained layer n limiting Boltzmann machine unit in sequence by adopting a back propagation method for parameter fine adjustment, and obtaining the trained deep confidence model.
S3, optimizing the structural parameters of the trained depth confidence model to obtain a depth confidence model with optimal structural parameters;
step S3 includes the following substeps:
s31, initializing an iteration parameter k, wherein k = 0, and taking the trained depth confidence model as a current optimized depth confidence model;
s32, calculating the fitness of the current optimized depth confidence model:
wherein,fin order to be a degree of fitness,Mfor the total number of verifications of the current optimized deep confidence model,mis as followsmThe result of the secondary verification is that,bin order to correctly classify the number of samples,cthe number of misclassified samples.
S33, judging whether the fitness meets a set threshold, if so, taking the current optimized depth confidence model as the depth confidence model with the optimal structural parameters, ending the substeps, if not, adding 1 to k, and jumping to the step S34;
s34, calculating the position and the speed of the structural parameter by adopting the parameter updating model, and carrying out the optimization of the kth iteration on the structural parameter of the current optimized depth confidence model based on the position and the speed of the structural parameter to obtain a kth suboptimal depth confidence model;
the parameter update model in step S34 is:
wherein,αin order to be the inertial weight,β 1is a first one of the acceleration factors, and,β 2is the second one of the acceleration factors, and,v ij k is as followskStructural parameters of sub-iterationiTo (1) ajThe speed of the dimensional variable is then determined,v ij k+1is as followsk+Structural parameters of 1 iterationiTo (1) ajThe speed of the dimensional variable is then determined,x ij k is as followskStructural parameters of sub-iterationiTo (1) ajThe position of the dimension-variable is,x ij k+1is as followsk+Structural parameters of 1 iterationiTo (1) ajThe position of the dimension-variable is,p ij k is as followskStructural parameters of sub-iterationiTo (1) ajThe optimal position of the individual extrema of the dimensional variable,r j k is as followskThe first of the sub-iterationsjThe global optimum position of the dimensional variable,a 1、a 2is a random number between 0 and 1.
S35, taking the k-th sub-optimal depth confidence model as the current optimal depth confidence model, and jumping to the step S32.
And S4, inputting the test set into the depth confidence model with the optimal structural parameters, and detecting the fault of the redundant strapdown inertial measurement unit.
As shown in fig. 3, a configuration scheme of a regular dodecahedron redundant strapdown inertial measurement unit is taken as an example to describe a method for detecting a fault of a redundant strapdown inertial measurement unit based on a parameter optimization depth confidence model: wherein O is the origin of coordinates, XYZ is three positiveM 1-m 6 are 6 inertial sensors, and the included angle between each inertial sensor and the coordinate axis isα。
Taking a gyroscope as an example, the fault types configured by the regular dodecahedron six-table redundant strapdown inertial measurement unit can be divided into: no. 1 gyro fault, No. 2 gyro fault, No. 3 gyro fault, No. 4 gyro fault, No. 5 gyro fault, No. 6 gyro fault and no fault.
The method is characterized in that a 4-layer depth confidence model structure is adopted, the output of six gyroscopes forms an input layer of a depth confidence model, and initial parameter hidden layers (the No. 1 limiting Boltzmann machine unit is outside a visible layer, and the rest are hidden layers) respectively comprise 20, 30, 10 and 7 neurons. Wherein 7 neurons in the last hidden layer respectively represent seven state characteristics of No. 1 gyro fault, No. 2 gyro fault, No. 3 gyro fault, No. 4 gyro fault, No. 5 gyro fault, No. 6 gyro fault, no fault and the like.
And after the training of the deep confidence model is finished by using the training set data, optimizing the structural parameters to obtain the optimal parameters. Inputting the test set data into a depth confidence model with optimal parameters, and checking the state of neurons contained in the last hidden layer:
if the state of the first neuron is 1, the No. 1 gyro is in failure, otherwise, the No. 1 gyro is not in failure; if the state of the second neuron is 1, the No. 2 gyro is in failure, otherwise, the No. 2 gyro is not in failure; if the state of the third neuron is 1, indicating that the No. 3 gyro fails, otherwise, indicating that the No. 3 gyro does not fail; if the state of the fourth neuron is 1, indicating that the No. 4 gyro fails, otherwise, indicating that the No. 4 gyro does not fail; if the state of the fifth neuron is 1, the No. 5 gyro is in failure, otherwise, the No. 5 gyro is not in failure; if the state of the sixth neuron is 1, indicating that the No. 6 gyro fails, otherwise, indicating that the No. 6 gyro does not fail; if the seventh neuron state is 1, all gyros are not in failure.
Claims (7)
1. A redundant strapdown inertial measurement unit fault detection method based on a parameter optimization depth confidence model is characterized by comprising the following steps:
s1, acquiring output data of the redundant strapdown inertial measurement unit, and constructing a training set and a test set based on the output data;
s2, training the deep confidence model by adopting a training set to obtain a trained deep confidence model;
s3, optimizing the structural parameters of the trained depth confidence model to obtain a depth confidence model with optimal structural parameters;
and S4, inputting the test set into the depth confidence model with the optimal structural parameters, and detecting the fault of the redundant strapdown inertial measurement unit.
2. The method for detecting the fault of the redundant strapdown inertial measurement unit based on the parameter-optimized depth confidence model according to claim 1, wherein the depth confidence model in the step S2 is composed of a plurality of layers of limiting boltzmann machine units, and the depth confidence model specifically comprises a layer 1 limiting boltzmann machine unit, a layer 2 limiting boltzmann machine unit, a layer 3 limiting boltzmann machine unit, a layer 4 limiting boltzmann machine unit, and a layer n limiting boltzmann machine unit which are connected in sequence.
3. The method for detecting the fault of the redundant strapdown inertial measurement unit based on the parameter optimized depth confidence model according to claim 2, wherein the step S2 comprises the following sub-steps:
s21, training the limiting Boltzmann machine units layer by layer to obtain all the limiting Boltzmann machine units after training;
s22, extracting features of the data output by the trained nth layer limiting Boltzmann machine unit to obtain an output result;
s23, comparing the output result with the actual value to obtain an error value;
and S24, distributing error values from the trained layer 1 limiting Boltzmann machine unit to the trained layer n limiting Boltzmann machine unit in sequence by adopting a back propagation method for parameter fine adjustment, and obtaining the trained deep confidence model.
4. The method for detecting the fault of the redundant strapdown inertial measurement unit based on the parameter optimized depth confidence model according to claim 3, wherein the step S21 comprises the steps of:
s211, initializing an iteration parameter r, wherein r = 1;
s212, inputting the training set into the 1 st layer of limiting Boltzmann machine unit, training the 1 st layer of limiting Boltzmann machine unit, updating the weight and the bias of the r layer of limiting Boltzmann machine unit, and obtaining the trained r layer of limiting Boltzmann machine unit;
s213, adding 1 to r, judging whether r is equal to n +1, if yes, finishing the training of all the limiting Boltzmann machine units, and if not, jumping to the step S212.
5. The method for detecting the fault of the redundant strapdown inertial measurement unit based on the parameter optimized depth confidence model according to claim 1, wherein the step S3 comprises the following sub-steps:
s31, initializing an iteration parameter k, wherein k = 0, and taking the trained depth confidence model as a current optimized depth confidence model;
s32, calculating the fitness of the current optimized depth confidence model;
s33, judging whether the fitness meets a set threshold, if so, taking the current optimized depth confidence model as the depth confidence model with the optimal structural parameters, ending the substeps, if not, adding 1 to k, and jumping to the step S34;
s34, calculating the position and the speed of the structural parameter by adopting the parameter updating model, and carrying out the optimization of the kth iteration on the structural parameter of the current optimized depth confidence model based on the position and the speed of the structural parameter to obtain a kth suboptimal depth confidence model;
s35, taking the k-th sub-optimal depth confidence model as the current optimal depth confidence model, and jumping to the step S32.
6. The method for detecting the fault of the redundant strapdown inertial measurement unit based on the parameter-optimized depth confidence model according to claim 5, wherein the formula for calculating the fitness of the current optimized depth confidence model in the step S32 is as follows:
wherein,fin order to be a degree of fitness,Mfor the total number of verifications of the current optimized deep confidence model,mis as followsmThe result of the secondary verification is that,bin order to correctly classify the number of samples,cthe number of misclassified samples.
7. The method for detecting the fault of the redundant strapdown inertial measurement unit based on the parameter optimized depth confidence model according to claim 5, wherein the parameter updating model in the step S34 is:
wherein,αin order to be the inertial weight,β 1is a first one of the acceleration factors, and,β 2is the second one of the acceleration factors, and,v ij k is as followskStructural parameters of sub-iterationiTo (1) ajThe speed of the dimensional variable is then determined,v ij k+1is as followsk+Structural parameters of 1 iterationiTo (1) ajThe speed of the dimensional variable is then determined,x ij k is as followskStructural parameters of sub-iterationiTo (1) ajThe position of the dimension-variable is,x ij k+1is as followsk+Structural parameters of 1 iterationiTo (1) ajThe position of the dimension-variable is,p ij k is as followskStructural parameters of sub-iterationiTo (1) ajThe optimal position of the individual extrema of the dimensional variable,r j k is as followskThe first of the sub-iterationsjThe global optimum position of the dimensional variable,a 1、a 2is a random number between 0 and 1.
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