Interface issues in hardware-in-the-loop simulation for spacecraft on-orbit docking

Tong Li Chang, Da Cheng Cong, Zheng Mao Ye, Jun Wei Han

科研成果: 书/报告/会议事项章节会议稿件同行评审

10 引用 (Scopus)

摘要

This paper presents an idea on the simulation/hardware interface of Hardware-In-the-Loop (HIL) simulation for spacecraft on orbit docking. The obstacles that hinder the design of the HIL simulation system are discussed. Then the design criteria of the HIL simulation system are presented based on them. Since the practical HIL simulation system for on orbit docking is very complicated, the verification about the criteria was done on 1 Degree-Of-Freedom (DOF) case with the nonlinear docking mechanism model. To put the design criteria into practice, the two-degree-of-freedom control structure is required as a control structure for the HIL simulation system for on-orbit docking. The relation ship between the distortion of the HEL simulation and the transfer characteristics of the simulation/hardware interface is qualitatively discussed. The simulation results on 1 DOF case demonstrated that the ideas and the methods discussed above are feasible and practical.

源语言英语
主期刊名2007 IEEE International Conference on Control and Automation, ICCA
出版商Institute of Electrical and Electronics Engineers Inc.
2584-2590
页数7
ISBN(印刷版)1424408180, 9781424408184
DOI
出版状态已出版 - 2007
已对外发布
活动2007 IEEE International Conference on Control and Automation, ICCA - Guangzhou, 中国
期限: 30 5月 20071 6月 2007

出版系列

姓名2007 IEEE International Conference on Control and Automation, ICCA

会议

会议2007 IEEE International Conference on Control and Automation, ICCA
国家/地区中国
Guangzhou
时期30/05/071/06/07

指纹

探究 'Interface issues in hardware-in-the-loop simulation for spacecraft on-orbit docking' 的科研主题。它们共同构成独一无二的指纹。

引用此