CN113375676B - Detector landing site positioning method based on impulse neural network - Google Patents

Detector landing site positioning method based on impulse neural network Download PDF

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CN113375676B
CN113375676B CN202110576033.0A CN202110576033A CN113375676B CN 113375676 B CN113375676 B CN 113375676B CN 202110576033 A CN202110576033 A CN 202110576033A CN 113375676 B CN113375676 B CN 113375676B
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CN113375676A (en
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袁家斌
查可可
马玮琦
李若玮
夏涛
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Nanjing University of Aeronautics and Astronautics
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/24Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 specially adapted for cosmonautical navigation
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06NCOMPUTING ARRANGEMENTS BASED ON SPECIFIC COMPUTATIONAL MODELS
    • G06N3/00Computing arrangements based on biological models
    • G06N3/02Neural networks
    • G06N3/04Architecture, e.g. interconnection topology
    • G06N3/045Combinations of networks
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06NCOMPUTING ARRANGEMENTS BASED ON SPECIFIC COMPUTATIONAL MODELS
    • G06N3/00Computing arrangements based on biological models
    • G06N3/02Neural networks
    • G06N3/04Architecture, e.g. interconnection topology
    • G06N3/049Temporal neural networks, e.g. delay elements, oscillating neurons or pulsed inputs
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06NCOMPUTING ARRANGEMENTS BASED ON SPECIFIC COMPUTATIONAL MODELS
    • G06N3/00Computing arrangements based on biological models
    • G06N3/02Neural networks
    • G06N3/08Learning methods
    • G06N3/084Backpropagation, e.g. using gradient descent

Abstract

The invention discloses a probe landing site positioning method based on a pulse neural network, which comprises the following steps of: preprocessing the meteorite pit DEM data on the surface of the star; training the training set data by adopting a U-Net network architecture based on an artificial neural network model ANN; converting UNET of the artificial neural network model ANN into UNET model of the impulse neural network model SNN; coding the image, and adopting an UNET model based on SNN to carry out test set detection; and (3) carrying out meteorite pit matching and positioning through a template matching algorithm, constructing a terrain road sign library, and realizing positioning. The invention realizes the positioning of the landing point of the detector by first applying the pulse neural network to the field of deep space detection and identifying the meteorite crater.

Description

Detector landing site positioning method based on impulse neural network
Technical Field
The invention belongs to the technical field of vision-based descending-section autonomous navigation of a spacecraft in a deep space exploration task, and particularly relates to a probe landing site positioning method based on a pulse neural network.
Background
After entering the 21 st century, the large aerospace state disputes develop a series of deep space exploration tasks, wherein the soft landing of the detector on the surface of the target star is realized, the safety of equipment and personnel is ensured, and the method is the basis for exploring deep space and developing aerospace technology in China. Typically, the probe positioning technology is through ground measurement and control stations or GNSS navigation technology. However, in a deep space environment, the technology has larger delay, and also has the problems of star shielding, signal transmission blocking and the like, so that the autonomous safe landing technology is a necessary technology for the future detector to land extraterrestrial satellites.
The accurate positioning of the landing points is an important basis for establishing a working coordinate system of the detector, provides position information for the subsequent navigation and scientific detection of the detector, and is an important premise for the detector to develop detection task work. However, the unpredictability of the environment of the extraterrestrial celestial body and the presence of obstructions such as merle pits or rock masses on the star floor present significant challenges to the safe landing of the detector. The current common methods are: computer vision-based landing zone location techniques find application in lunar, mars, and other asteroid exploration tasks. In the goddess Chang E task II, landing points are resolved by using landing camera images, navigation camera images and digital orthophotos, but the positioning result is completed in a few hours after the detector falls into the month; chang's III combines with the very long baseline interferometry technique to locate landing sites; and the goddess Chang E No. four landing zone is the back of moon, because the star shielding, traditional ranging, speed measuring and VLBI technology can not be used in the power reduction stage of the detector, the landing zone positioning is realized on the basis of high-precision image and geometric transformation by adopting a computer vision method. However, the above methods have a problem of real-time performance.
The closest approach to the method is a landing zone positioning technology based on a landform landmark database, namely, a landing image acquired in a descending stage is identified through a convolutional neural network, and the landform landmark database is established through identifying barriers such as merle pits and rocks contained in the image, so that landing point positioning is realized. However, in order to improve the accuracy of the model, a deeper neural network and a large number of data sets are required to perform model training, which brings about a large amount of energy consumption loss and also has a real-time problem.
Disclosure of Invention
The invention provides a method for positioning a landing point of a detector based on a pulse neural network, which solves the problems of larger time delay, low accuracy and higher energy consumption of the existing landing point positioning method.
In order to achieve the above purpose, the invention adopts the following technical scheme:
a probe landing site positioning method based on a pulse neural network comprises the following steps:
s1, preprocessing the data of the meteorite crater DEM on the surface of a star;
s2, training set data by adopting a U-Net network architecture based on an artificial neural network model (artificial neural network, ANN);
s3, converting the UNET of the artificial neural network model ANN into a UNET model of a pulse neural network model (SNN);
s4, encoding the image, and detecting a test set by adopting an UNET model based on SNN;
s5, performing merle pit matching and positioning through a template matching algorithm, constructing a terrain road sign library, and realizing positioning.
Further, the step S1 specifically includes:
s11, the original data set is 184340 x 61440 pixels and 16 bits/pixel, firstly downsampling (down-sampled) is carried out on the original data set to convert the original data set into 92160 x 30720 pixels and 8 bits/pixel data;
s12, randomly cutting the DEM image in the S11 into square areas, and converting the square areas into 256-256 pixel data sets through downsampling;
s13, orthographic projection is carried out on the image in the S12, and other parts are filled with zero;
s14, linearly scaling the image in the S13, and improving the contrast of the image to obtain an input data set;
s15, converting the information into 256-by-256 pixel output labels according to the longitude and latitude and the radius information of the meteorite crater.
Further, the step S2 specifically includes:
s21, inputting the 256-by-256-bit pixel data set constructed in the S14 into an image segmentation network UNET, wherein the left side of the network is a coding layer (decoder), and the right side of the network is a decoding layer (decoder); firstly, carrying out downsampling through 4 blocks 1, wherein each block1 is downsampled by 3 effective convolutions and 1 max pooling, so as to obtain a characteristic diagram; then up-sampling is carried out through 4 blocks 2 to improve the resolution ratio, and then up-sampling results are connected with network left coding layer results through jump connection, so that deep features and shallow features are combined, images are thinned, and feature images are obtained;
s22, predicting the feature map obtained in the S21, and judging whether the current position is the meteorite pit boundary or not through a convolution kernel of 1*1, so as to obtain a 256-by-256-bit pixel value prediction map (predicted mask). However, the output result does not contain information such as the position, the radius and the like of the meteorite crater, so that a template matching algorithm in S5 is also needed, and the specific longitude and latitude information of the identified meteorite crater is used for constructing a landmark library.
Further, the step S3 specifically includes:
s31, acquiring a trained UNET model in S22, and converting model weight W and bias B through scale factors (scales) to ensure that pulse signals exist in a deep network; let us assume that there is a layer of l in UNET, where l e {1,2, 3..l-1, l }, W l ann And b l ann For trained ANN-based network layer I weights and biases, W l snn And b l snn For the scaled weight and bias of the first layer of SNN network, acquiring the activation value { a } l 1 ,a l 2 ,a l 3 .., and remembering a maximum activation value of lambda l =max{a l 1 ,a l 2 ,a l 3 .. the scaling factor of each layer is the ratio between the maximum activation value of the previous layer and the maximum activation value of the current layer, i.e. the scaling factor scale of the first layer l Maximum activation value lambda for layer l-1 l-1 Divided by the maximum activation value lambda of the first layer l ,scale l =λ l-1l The method comprises the steps of carrying out a first treatment on the surface of the W is then l snn =W l ann *scale l ,b l snn =b l annl
S32, the activation value of each layer in the traditional neural network is required to be encoded in the impulse neural network and converted into discrete impulses; in the leaky-distributed integral neuron model (Leaky integrate fire, LIF), assuming a total time window of T, the voltage value V at the first layer, time T mem,j l (t) is the voltage value V at the previous time t-1 mem,j l (t-1) And the input current z at the current time t j l (t), i.e. V mem,j l (t)=V mem,j l (t-1)+z j l (t) wherein:θ i l (t)=U(V mem,i l (t)-V th ),w i,j l representing the weight of neuron i connected to neuron j of the first layer, where i represents a neuron in the previous layer of neuron l-1, θ i l-1 (t) shows whether or not the layer 1 neuron i is pulsed at time t, V th Is threshold, U is a step function, θ i l (t) indicates whether the first layer neuron i is pulsed at time t, and the value is 0 or 1, and the current voltage value exceeds the threshold value V th When then theta i l (t) 1 and resetting the voltage value to 0, if the current voltage value has not reached the threshold value, θ i l (t) 0, the voltage value continues to accumulate until a pulse can be triggered;
s33, counting the total number of pulses issued by each output neuron in the total time window T in the last layer, and converting the total number of pulses into pixel values of an output image to obtain a prediction result.
Further, the step S4 specifically includes:
s41, because in the pulse neural network, the input and the activation value of each layer are transmitted in the form of pulse signals, the input image is required to be encoded; the common encoding method of the input image is a poisson encoding method, namely, in a time window T with a certain length, the number of pulses issued by the input neurons corresponding to each pixel is distributed in poisson, and the formula is as follows:wherein: p denotes the probability of issuing k pulses within the total time window T; x is the case of issuing k pulses; k is the number of excitation pulses; μ is the excitation frequency proportional to the pixel value; e is the base of the natural logarithm, here taking the value 2.718, then within the total time window T,each cycle is multiplied by the probability of the time step dt of each simulation by the excitation frequency to determine whether a pulse is issued, and the dt is usually 1, so that a frequency code is finally formed;
s42, transmitting the input pulse sequence into a pulsed UNET model to obtain an image segmentation result.
Further, the step S5 specifically includes:
s51, the merle pit obtained through image segmentation in the S4 is subjected to a template matching algorithm (match-template) to obtain the position and the radius of the current merle pit, namely a landmark library based on the merle pit is obtained, and the detector obtains the current position by identifying the information of the current merle pit;
s52, screening and detecting repeated merle pits by comparing the obtained position and radius information, and perfecting a road sign warehouse based on the merle pits.
Compared with the prior art, the invention has the following beneficial effects:
the invention realizes the positioning of the landing point of the detector by first applying the pulse neural network to the field of deep space detection and identifying the meteorite crater. Firstly, processing the DEM image to obtain an image and a label required by training and testing; training a traditional artificial intelligence UNET model by using a training set, and converting the trained UNET model into a pulse neural network version (Spiking-UNET, SUNET); and finally, using a template matching algorithm to find out the specific longitude and latitude information and the radius of each meteorite crater, thereby realizing the positioning based on a road sign library. The invention has the advantages that the impulse neural network is an event-driven mechanism, and only the impulse release is the loss of energy consumption, so that the energy consumption can be greatly reduced; meanwhile, experiments show that the convolution kernel is 3*3, so that the detection effect of the UNET network on the merle pit with larger radius is poor, and SUNET can solve the problem, and the integrity of a terrain library and the positioning accuracy are improved.
Drawings
FIG. 1 is a flow chart of the present invention.
Fig. 2 is a flowchart for converting CNN to SNN.
FIG. 3 is a map of the merle-pit detection network SUNET model based on a pulsed neural network.
Detailed Description
The invention will be further illustrated with reference to examples.
As shown in fig. 1, a deep space probe landing site positioning method based on a pulse neural network comprises the following steps:
s1, preprocessing the data of the meteorite crater DEM on the surface of a star;
s11, the original data set is 184340 x 61440 pixels and 16 bits/pixel, firstly downsampling (down-sampled) is carried out on the original data set to convert the original data set into 92160 x 30720 pixels and 8 bits/pixel data;
s12, randomly cutting the DEM image in the S11 into square areas, and converting the square areas into 256-256 pixel data sets through downsampling;
s13, orthographic projection is carried out on the image in the S12, and other parts are filled with zero;
s14, linearly scaling the image in the S13, and improving the contrast of the image to obtain an input data set;
s15, converting the information into 256-by-256 pixel output labels according to the longitude and latitude and the radius information of the meteorite crater.
S2, training set data by adopting a U-Net network architecture based on an artificial neural network model (artificial neural network, ANN);
s21, inputting the 256-by-256-bit pixel data set constructed in the S14 into an image segmentation network UNET, wherein the left side of the network is an encoding layer (decoder), and the right side of the network is a decoding layer (decoder). Firstly, carrying out downsampling through 4 blocks 1, wherein each block1 is downsampled by 3 effective convolutions and 1 max pooling, so as to obtain a characteristic diagram; and then up-sampling is carried out through 4 blocks 2 to improve the resolution, and then the up-sampling result is connected with the network left coding layer result through jump connection, so that the combination of deep features and shallow features is realized, the image is thinned, and a feature map is obtained.
S22, predicting the feature map obtained in the S21, and judging whether the current position is the meteorite pit boundary or not through a convolution kernel of 1*1, so as to obtain a 256-by-256-bit pixel value prediction map (predicted mask). However, the output result does not contain information such as the position, the radius and the like of the meteorite crater, so that a template matching algorithm in S5 is also needed, and the specific longitude and latitude information of the identified meteorite crater is used for constructing a landmark library.
Specifically, as shown in fig. 2, the image segmentation architecture based on the conventional neural network is trained first, and then the model is converted into the SNN architecture after mapping conversion from ANN to SNN. The main framework of the merle segmentation model of the network model M adopts a U-Net network with good effect on image segmentation, wherein the U-Net network comprises 4 layers of downsampling, each layer comprises 2 convolution kernels of 3*3, feature extraction is carried out, and 2 x 2 average pooling is carried out on the layers for downsampling. After 4-layer downsampling, reduction is performed by 4-layer upsampling. By 2 x 2 up-convolutions between layers, information is supplemented by skip connection because there is information loss in each up-convolution, and each layer contains 2 3*3 convolution kernels, and the last layer outputs the prediction result for each layer. Comparing the predicted result with the label data through a Dice loss functionWherein: x represents a predicted value, y represents a real value, x is equal to y represents a part where the predicted value and the real value coincide, x is equal to y represents a sum of the predicted value and the real value, the smaller the loss function L value is, the more accurate the segmentation result is represented, the weight is continuously adjusted through back propagation, and finally the loss function value is minimum, so that a final training model is obtained.
S3, converting the UNET of the artificial neural network model ANN into a UNET model of a pulse neural network model (SNN);
s31, acquiring a trained UNET model in S22, wherein in order to ensure that pulse signals exist in a deep network, model weights W and offsets B are converted through scale factors (scales); let us assume that there is a layer of l in UNET, where l e {1,2, 3..l-1, l }, W l ann And b l ann For trained ANN-based network layer I weights and biases, W l snn And b l snn For the scaled weight and bias of the first layer of SNN network, acquiring the activation value { a } l 1 ,a l 2 ,a l 3 .., and remembering a maximum activation value of lambda l =max{a l 1 ,a l 2 ,a l 3 .. the scaling factor of each layer is the ratio between the maximum activation value of the previous layer and the maximum activation value of the current layer, i.e. the scaling factor scale of the first layer l Maximum activation value lambda for layer l-1 l-1 Divided by the maximum activation value lambda of the first layer l ,scale l =λ l-1l The method comprises the steps of carrying out a first treatment on the surface of the W is then l snn =W l ann *scale l ,b l snn =b l annl
S32, the activation value of each layer in the traditional neural network is required to be encoded in the impulse neural network and converted into discrete impulses; in the leaky-distributed integral neuron model (Leaky integrate fire, LIF), assuming a total time window of T, the voltage value V at the first layer, time T mem,j l (t) is the voltage value V at the previous time t-1 mem,j l Input current z at (t-1) and current time t j l (t), i.e. V mem,j l (t)=V mem,j l (t-1)+z j l (t) wherein:θ i l (t)=U(V mem,i l (t)-V th ),w i,j l representing the weight of neuron i connected to neuron j of the first layer, where i represents a neuron in the previous layer of neuron l-1, θ i l-1 (t) shows whether or not the layer 1 neuron i is pulsed at time t, V th Is threshold, U is a step function, θ i l (t) indicates whether the first layer neuron i is pulsed at time t, and the value is 0 or 1, and the current voltage value exceeds the threshold value V th When then theta i l (t) 1 and resetting the voltage value to 0, if the current voltage value has not reached the threshold value, θ i l (t) 0, the voltage value continues to accumulate until a pulse can be triggered;
s33, counting the total number of pulses issued by each output neuron in the total time window T in the last layer, and converting the total number of pulses into pixel values of an output image to obtain a prediction result.
Specifically, converting the traditional neural network model into a pulsed neural network includes: image pulsing, weight mapping, convolution layer and upsampling layer pulsing, as shown in fig. 3. To avoid too many or how many pulses are in the network, the weights are mapped. The DEM image (input DEM) is then poisson encoded and converted into a pulse input network. Image compression is carried out on the left side of the network, the network comprises 4 layers in total, each layer comprises 2 convolution kernels, the weight value in each convolution kernel is obtained by mapping the weight value in S2, and in a time window T, whether the neuron emits a pulse to enter the next layer at the current moment is judged by calculating a voltage value through a spiking-relu function; the average sampling based on the pulse neural network is adopted between the layers, and the pulse average value at the current moment is counted; the right side of the network performs image decoding, which also includes 4 layers, firstly restores through an up-sampling layer based on SNN, supplements image information through jump connection in order to reduce image information loss, and finally outputs a prediction result (predicted mask).
S4, coding the image, and detecting merle pits by adopting an UNET model based on SNN;
s41, because in the pulse neural network, the input and the activation value of each layer are transmitted in the form of pulse signals, the input image is required to be encoded; the common encoding method of the input image is a poisson encoding method, namely, in a time window T with a certain length, the number of pulses issued by the input neurons corresponding to each pixel is distributed in poisson, and the formula is as follows:wherein: p denotes the probability of issuing k pulses within the total time window T; x is the case of issuing k pulses; k is the number of excitation pulses; μ is the excitation frequency proportional to the pixel value; e is the base of the natural logarithm, here taking the value 2.718, then each cycle is multiplied by each modulus at the excitation frequency within the total time window TThe probability of the quasi-time step dt determines whether a pulse is issued, and the dt is generally 1, and finally a frequency code is formed; .
S42, transmitting the input pulse sequence into a pulsed UNET model to obtain an image segmentation result.
S5, performing merle pit matching and positioning through a template matching algorithm, constructing a terrain road sign library, and realizing positioning.
S51, the merle pit obtained through image segmentation in the S4 is subjected to a template matching algorithm (match-template) to obtain the position and the radius of the current merle pit, so that a landmark library based on the merle pit can be obtained, and the detector can obtain the current position by identifying the information of the current merle pit.
S52, screening and detecting repeated merle pits by comparing the obtained position and radius information, and perfecting a road sign warehouse based on the merle pits.
The foregoing is only a preferred embodiment of the invention, it being noted that: it will be apparent to those skilled in the art that various modifications and adaptations can be made without departing from the principles of the present invention, and such modifications and adaptations are intended to be comprehended within the scope of the invention.

Claims (6)

1. The method for positioning the landing site of the detector based on the impulse neural network is characterized by comprising the following steps of:
s1, preprocessing the data of the meteorite crater DEM on the surface of a star;
s2, training the training set data by adopting a U-Net network architecture based on an artificial neural network model ANN;
s3, converting the UNET of the artificial neural network model ANN into a UNET model of the impulse neural network model SNN;
the step S3 includes a step S31,
s31, acquiring a trained UNET model in the S2, and converting model weight W and bias B through scaling factors to ensure that pulse signals exist in a deep network; let us assume that there is a layer of l in UNET, where l ε {1,2,3 … l-1, l }, W l ann And b l ann For trained basesWeights and biases at layer I of ANN network, W l snn And b l snn For the scaled weight and bias of the first layer of SNN network, acquiring the activation value { a } l 1 ,a l 2 ,a l 3 .., and remembering a maximum activation value of lambda l =max{a l 1 ,a l 2 ,a l 3 .. the scaling factor of each layer is the ratio between the maximum activation value of the previous layer and the maximum activation value of the current layer, i.e. the scaling factor scale of the first layer l Maximum activation value lambda for layer l-1 l-1 Divided by the maximum activation value lambda of the first layer l ,scale l =λ l-1l The method comprises the steps of carrying out a first treatment on the surface of the W is then l snn =W l ann *scale l ,b l snn =b l annl
S4, encoding the image, and detecting a test set by adopting an UNET model based on SNN;
s5, performing merle pit matching and positioning through a template matching algorithm, constructing a terrain road sign library, and realizing positioning.
2. The method for positioning a probe landing site based on a pulsed neural network according to claim 1, wherein the step S1 is specifically:
s11, an original data set is 184340 x 61440 pixels and 16bit/pixel, firstly downsampling is carried out on the original data set, and downsampling is carried out on the original data set to convert the original data set into 92160 x 30720 pixels and 8bit/pixel data;
s12, randomly cutting the DEM image in the S11 into square areas, and converting the square areas into 256-256 pixel data sets through downsampling;
s13, orthographic projection is carried out on the image in the S12, and other parts are filled with zero;
s14, linearly scaling the image in the S13, and improving the contrast of the image to obtain an input data set;
s15, converting the information into 256-by-256 pixel output labels according to the longitude and latitude and the radius information of the meteorite crater.
3. The method for positioning the probe landing site based on the impulse neural network according to claim 2, wherein the step S2 specifically comprises:
s21, inputting the 256-by-256-bit pixel data set constructed in the S14 into an image segmentation network UNET, wherein the left side of the network is a coding layer decoder, and the right side of the network is a decoding layer decoder; firstly, carrying out downsampling through 4 blocks 1, wherein each block1 is downsampled by 3 effective convolutions and 1 max pooling, so as to obtain a characteristic diagram; then up-sampling is carried out through 4 blocks 2 to improve the resolution ratio, and then up-sampling results are connected with network left coding layer results through jump connection, so that deep features and shallow features are combined, images are thinned, and feature images are obtained;
s22, predicting the feature map obtained in the S21, and judging whether the current position is the meteorite pit boundary or not through a convolution kernel of 1*1, so as to obtain a 256-by-256-bit pixel value predicted mask; however, the output result does not contain the position and radius information of the meteorite crater, so that a template matching algorithm in S5 is also needed, and the specific longitude and latitude information of the identified meteorite crater is needed, so that a landmark library is constructed.
4. The method for positioning a probe landing site based on a pulsed neural network according to claim 3, wherein the step S3 is specifically:
s31, acquiring a UNET model trained in the S22, and converting model weight W and bias B through scaling factors to ensure that pulse signals exist in a deep network; let us assume that there is a layer of l in UNET, where l ε {1,2,3 … l-1, l }, W l ann And b l ann For trained ANN-based network layer I weights and biases, W l snn And b l snn For the scaled weight and bias of the first layer of SNN network, acquiring the activation value { a } l 1 ,a l 2 ,a l 3 .., and remembering a maximum activation value of lambda l =max{a l 1 ,a l 2 ,a l 3 .. the scaling factor of each layer is the one of the preceding layerThe ratio between the maximum activation value and the maximum activation value of the current layer, i.e. the scale factor of the first layer l Maximum activation value lambda for layer l-1 l-1 Divided by the maximum activation value lambda of the first layer l ,scale l =λ l-1l The method comprises the steps of carrying out a first treatment on the surface of the W is then l snn =W l ann *scale l ,b l snn =b l annl
S32, the activation value of each layer in the traditional neural network is required to be encoded in the impulse neural network and converted into discrete impulses; in the leakage issue integral neuron model, assuming that the total time window is T, the voltage value V at the first layer and the T moment mem,j l (t) is the voltage value V at the previous time t-1 mem,j l Input current z at (t-1) and current time t j l (t), i.e. V mem,j l (t)=V mem,j l (t-1)+z j l (t) wherein:θ i l (t)=U(V mem,i l (t)-V th ),w i,j l representing the weight of neuron i connected to neuron j of the first layer, where i represents a neuron in the previous layer of neuron l-1, θ i l-1 (t) shows whether or not the layer 1 neuron i is pulsed at time t, V th Is threshold, U is a step function, θ i l (t) indicates whether the first layer neuron i is pulsed at time t, and the value is 0 or 1, and the current voltage value exceeds the threshold value V th When then theta i l (t) 1 and resetting the voltage value to 0, if the current voltage value has not reached the threshold value, θ i l (t) 0, the voltage value continues to accumulate until a pulse can be triggered;
s33, counting the total number of pulses issued by each output neuron in the total time window T in the last layer, and converting the total number of pulses into pixel values of an output image to obtain a prediction result.
5. The method for positioning a probe landing site based on a pulsed neural network according to claim 4, wherein the step S4 is specifically:
s41, because in the pulse neural network, the input and the activation value of each layer are transmitted in the form of pulse signals, the input image is required to be encoded; the common encoding method of the input image is a poisson encoding method, namely, in a time window T with a certain length, the number of pulses issued by the input neurons corresponding to each pixel is distributed in poisson, and the formula is as follows:wherein: p denotes the probability of issuing k pulses within the total time window T; x is the case of issuing k pulses; k is the number of excitation pulses; μ is the excitation frequency proportional to the pixel value; e is a base number of natural logarithms, and in a total time window T, determining whether pulses are issued or not according to the probability that the excitation frequency is multiplied by the time step dt of each simulation in each cycle, and taking 1 for dt to finally form a frequency code;
s42, transmitting the input pulse sequence into a pulsed UNET model to obtain an image segmentation result.
6. The method for positioning a probe landing site based on a pulsed neural network according to claim 5, wherein the step S5 is specifically:
s51, the position and the radius of the current meteorite pit are obtained through a template matching algorithm by the meteorite pit obtained through image segmentation in the S4, namely a landmark library based on the meteorite pit is obtained, and the detector obtains the current position by identifying the information of the current meteorite pit;
s52, screening and detecting repeated merle pits by comparing the obtained position and radius information, and perfecting a road sign warehouse based on the merle pits.
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CN114519723A (en) * 2021-12-24 2022-05-20 上海海洋大学 Meteorite crater automatic extraction method based on pyramid image segmentation
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Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019104767A1 (en) * 2017-11-28 2019-06-06 河海大学常州校区 Fabric defect detection method based on deep convolutional neural network and visual saliency
CN110210563A (en) * 2019-06-04 2019-09-06 北京大学 The study of pattern pulse data space time information and recognition methods based on Spike cube SNN
CN111652896A (en) * 2020-05-29 2020-09-11 北京理工大学 Inertial navigation auxiliary meteorite crater coarse-to-fine detection method
CN112580502A (en) * 2020-12-17 2021-03-30 南京航空航天大学 SICNN-based low-quality video face recognition method
CN112819794A (en) * 2021-02-04 2021-05-18 青岛科技大学 Small celestial body meteorite crater detection method based on deep learning

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102019212907A1 (en) * 2019-08-28 2021-03-04 Robert Bosch Gmbh Method, device and computer program for creating a pulsed neural network

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019104767A1 (en) * 2017-11-28 2019-06-06 河海大学常州校区 Fabric defect detection method based on deep convolutional neural network and visual saliency
CN110210563A (en) * 2019-06-04 2019-09-06 北京大学 The study of pattern pulse data space time information and recognition methods based on Spike cube SNN
CN111652896A (en) * 2020-05-29 2020-09-11 北京理工大学 Inertial navigation auxiliary meteorite crater coarse-to-fine detection method
CN112580502A (en) * 2020-12-17 2021-03-30 南京航空航天大学 SICNN-based low-quality video face recognition method
CN112819794A (en) * 2021-02-04 2021-05-18 青岛科技大学 Small celestial body meteorite crater detection method based on deep learning

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
基于深度学习的大型陨石坑识别方法研究;郑磊等;《北京航空航天大学学报》;第46卷(第5期);第994-1003页 *

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