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Three-Impulse Model for Spacecraft to Avoid Space Debris and Return to the Original Orbit

Ming Wen Shaozhao Lu Yao Zhang Hongbo Wang Ji Ye

空间科学与技术(英文)2025,Vol.2025Issue(4):343-353,11.
空间科学与技术(英文)2025,Vol.2025Issue(4):343-353,11.DOI:10.34133/space.0266

Three-Impulse Model for Spacecraft to Avoid Space Debris and Return to the Original Orbit

Three-Impulse Model for Spacecraft to Avoid Space Debris and Return to the Original Orbit

Ming Wen 1Shaozhao Lu 2Yao Zhang 1Hongbo Wang 1Ji Ye1

作者信息

  • 1. School of Aerospace Engineering,Beijing Institute of Technology,Beijing 100081,China
  • 2. Institute of Telecommunication and Navigation Satellite,China Academy of Space Technology,Beijing 100094,China
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摘要

引用本文复制引用

Ming Wen,Shaozhao Lu,Yao Zhang,Hongbo Wang,Ji Ye..Three-Impulse Model for Spacecraft to Avoid Space Debris and Return to the Original Orbit[J].空间科学与技术(英文),2025,2025(4):343-353,11.

基金项目

This work was supported by the National Natural Science Foundation of China under grant U21B6001. ()

空间科学与技术(英文)

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