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《Acta Armamentarii》 1991-01
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APPLICATION OF THE QUATERNION METHOD IN FLIGHT TRAJECTORY SIMULATION OF TACTICAL MISSILES

Zheng Xiaoyu Qiam Xingfang (Beijing Institute of Technology)  
This paper discusses the application of quaternion method in the simulation of vertically launched tactical missiles and rocket-throwing submtssiles. Equation derivation, computations and analysis for in-flight trajectory simulation of an anti-tank missile and a ship-to-air missile are also given
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【Co-citations】
Chinese Journal Full-text Database 10 Hits
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China Proceedings of conference Full-text Database 1 Hits
1 Li Baokun~1 Cao Yi~2 Huang Zhen~3 Zhang Wenxiang~1 Zhang Lingyun~3 (~1Department of Mechanical Engineering,Anhui University of Science and Technology ~2 College of Mechanical Engineering of Southern Yangtze University ~3College of Mechanical Engineering of Yanshan University );Orientation Capability Analysis of Stewart Manipulator Using Unit Quaternion[A];[C];2006
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