@inproceedings{9ae9b96ffde54df09e4370382807b9b9,
title = "Design of multidimensional space motion simulation system for spacecraft attitude and orbit guidance and control based on radar RF environment",
abstract = "The hardware-in-the-loop (HIL) simulation system of spacecraft attitude and orbit control has been studied. In this paper, the composing of the HIL system and the main functions of sub-systems are given. The method to determine the scaling ratio of a simulation system is introduced. A novel communication scheme is designed based on optical reflective fiber memory. The details to design a GNC/dynamic simulator including their working flow is developed. Finally, the ground monitor sub-system is discussed. The design and develop of HIL simulation system provides a basic platform for ground HIL simulation of spacecraft.",
keywords = "Monitor system, Scaling ratio, Simulation, Spacecraft",
author = "Zhijun Lu and Hongwei Xia and Guangcheng Ma and Changhong Wang and Shengqing Yang",
note = "Publisher Copyright: {\textcopyright} 2016 IEEE.; 6th International Conference on Instrumentation and Measurement, Computer, Communication and Control, IMCCC 2016 ; Conference date: 21-07-2016 Through 23-07-2016",
year = "2016",
month = dec,
day = "5",
doi = "10.1109/IMCCC.2016.190",
language = "英语",
series = "Proceedings - 2016 6th International Conference on Instrumentation and Measurement, Computer, Communication and Control, IMCCC 2016",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "28--32",
editor = "Junbao Li",
booktitle = "Proceedings - 2016 6th International Conference on Instrumentation and Measurement, Computer, Communication and Control, IMCCC 2016",
address = "美国",
}