月球立方星姿态控制系统的初步设计与测试

Translated title of the contribution: Preliminary design and test of attitude control system for lunar CubeSats

Chihang Yang, Jiangkai Liu, Long Long, Huan Song, Long Li, Lingchao Zhu, Bingxu Ye, Hongru Chen, Hao Zhang

Research output: Contribution to journalArticlepeer-review

1 Citation (Scopus)

Abstract

CubeSats are miniature functional satellites. The increasing interest in CubeSats has uncovered the potential for planetary missions. Besides, CubeSats is an excellent educational platform. The preliminary attitude control system is designed and the corresponding hardware is built using commercial products for a lunar mission employing a CubeSat constellation to provide positioning service for landers/rovers on the far side of the moon. At the same time, the basic frame and necessary subsystems including the structure, power and on-board computer subsystems, and the attitude experiment platform are constructed. Based on the hardware platform, the control model is deeply understood through measuring damping coefficients by experiments. A PD control method is designed to control the attitude. The numerical and physical simulation results match well, and the CubeSat system achieves accurate attitude maneuver.

Translated title of the contributionPreliminary design and test of attitude control system for lunar CubeSats
Original languageChinese (Traditional)
Pages (from-to)28-35
Number of pages8
JournalChinese Space Science and Technology
Volume39
Issue number4
DOIs
Publication statusPublished - Aug 25 2019
Externally publishedYes

All Science Journal Classification (ASJC) codes

  • Materials Science(all)
  • Aerospace Engineering
  • Electrical and Electronic Engineering

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