Detector landing point positioning method based on spiking neural network

A technology of pulse neural network and positioning method, which is applied in the field of detector landing point positioning based on pulse neural network, which can solve the problems of high energy consumption, low accuracy, and large time delay

Pending Publication Date: 2021-09-10
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The invention provides a detector landing point positioning method based on a pulse neural network to solve the problems of large time delay, low accuracy and high energy consumption in the existing landing point positioning methods. By using the pulse neural network , to identify the craters on the surface of the star, so as to realize the positioning of the landing zone

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  • Detector landing point positioning method based on spiking neural network
  • Detector landing point positioning method based on spiking neural network
  • Detector landing point positioning method based on spiking neural network

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Embodiment Construction

[0037] Below in conjunction with embodiment the present invention will be further described.

[0038] Such as figure 1 As shown, a method for locating the landing site of a deep space probe based on a spiking neural network includes the following steps:

[0039] S1. Preprocessing the crater DEM data on the surface of the star;

[0040] S11. The original data set is 184320*61440 pixels, 16bit / pixel, first down-sampled to convert it into 92160*30720 pixels, 8bit / pixel data;

[0041] S12. Randomly crop the DEM image in S11 into a square area, and convert it into a data set of 256*256 pixels by downsampling;

[0042] S13. Orthoprojecting the image in S12, and filling other parts with zeros;

[0043] S14. Linearly zoom the image in S13, improve the image contrast, and obtain the input data set;

[0044] S15. Convert it into an output label of 256*256 pixels according to the longitude, latitude and radius information of the crater.

[0045] S2. Using the U-Net network architect...

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Abstract

The invention discloses a detector landing point positioning method based on a pulse neural network. The method comprises the following steps: preprocessing meteorite crater DEM data on the surface of a star; training a training set data by adopting a U-Net network architecture based on an artificial neural network model ANN; converting the UNET of the artificial neural network model ANN into a UNET model of a pulse neural network model SNN; coding the image, and carrying out test set detection by adopting the UNET model based on SNN; and carrying out meteorite crater matching and positioning through a template matching algorithm, and constructing a terrain landmark library to realize positioning. The spiking neural network is applied to the field of deep space exploration for the first time, and positioning of the landing point of the detector is achieved by identifying the meteorite crater.

Description

technical field [0001] The invention belongs to the technical field of vision-based descent segment autonomous navigation of spacecraft in deep space exploration missions, and in particular relates to a method for locating a landing point of a probe based on a pulse neural network. Background technique [0002] After entering the 21st century, the space powers have launched a series of deep space exploration missions. Among them, realizing the soft landing of the probe on the surface of the target star to ensure the safety of equipment and personnel is the basis for our country to explore deep space and develop aerospace technology. Usually, the detector positioning technology is through the ground measurement and control station or GNSS navigation technology. However, in the deep space environment, this technology has a large delay, and there are also problems such as star occlusion and signal transmission blockage. Therefore, autonomous safe landing technology is a necessa...

Claims

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Application Information

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Patent Type & AuthorityApplications(China)
IPC IPC(8): G01C21/24G06N3/04G06N3/08
CPCG01C21/24G06N3/049G06N3/084G06N3/045
Inventor袁家斌查可可马玮琦李若玮夏涛
OwnerNANJING UNIV OF AERONAUTICS & ASTRONAUTICS