NDLI: Design and realization of the high accuracy attitude and orbit control real-time simulation platform for spacecraft

Content Provider	IEEE Xplore Digital Library
Author	Gao Yudong Min Hu Guoqiang Zeng
Copyright Year	2011
Description	Author affiliation: The Academy of Equipment Command & Technology, Beijing, China (Min Hu; Guoqiang Zeng) \|\| Institute of Aerospace and Material Engineering, National University of Defense Technology, Changsha, China (Gao Yudong)
Abstract	To verify the correctness and real-time performance of the high accuracy attitude and orbit control algorithms for spacecraft mission, the attitude and orbit control software is developed based on the embedded real-time VxWorks operation system, and based on the high accuracy attitude and orbit dynamic simulation software, aground real-time simulation platform is established. The software as well as hardware architecture and interface of the simulation platform are introduced. The key problems are solved, including the synchronization and data communication between the onboard computer and the dynamic simulation computer, and the wireless communication between the on-board computer and the ground control center. The simulation result shows that reliability and real time of the platform can meet the requirements, and the platform provides a good support environment for the attitude and orbit control ground test and performance evaluation for spacecrafts.
Starting Page	233
Ending Page	236
File Size	178490
Page Count	4
File Format	PDF
ISBN	9781424487271
e-ISBN	9781424487288
DOI	10.1109/CSAE.2011.5952460
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2011-06-10
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Real-time simulation platform On-board computer CAN bus Attitude and orbit control for spacecraft
Content Type	Text
Resource Type	Article

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