Parachute Deployment Fault Identification and Landing Point Prediction of Spacecraft Recovery System Based on Swin Transformer and Edge Detection-Reference-Cited by-同舟云学术

Parachute Deployment Fault Identification and Landing Point Prediction of Spacecraft Recovery System Based on Swin Transformer and Edge Detection

Published:2022-11-25 Issue: Volume: Page:
ISSN:
Container-title:2022 5th International Conference on Mechatronics, Robotics and Automation (ICMRA)
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Author:

Bai Yilan¹,Hu Qibin²,Long Yu¹,Ma Ke¹,Zhao Chuangye¹,Zhang Mengying¹

Affiliation:

1. National University of Defense Technology,College of Aerospace Science and Engineering,Changsha,P.R.China

2. National University of Defense Technology,College of Electronic Science and Engineering,Changsha,P.R.China

Funder

National University of Defense Technology

Publisher

IEEE

Link

Reference20 articles.

1. Research on prediction of skip entry spacecraft's landing site[J];boyang;Journal of Nanjing University of Aeronautics & Astronautics,2021

2. Parachute Recovery Systems Design Manual[R];knacke;ADA247666,0

3. Calculation Methods of Added Mass of Parachute[J];huang;Spacecraft Recovery & Remote Sensing,2016

4. A novel approach for color image edge detection using multidirectional Sobel filter on HSV color space[J];bora;Int J Comput Sci,2017

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