@inproceedings{9155f4b1048649459ba5df62a6f4ff94,
title = "The application of linear adjoint method in rocket ballistic error analysis",
abstract = "This paper established a linear dynamic model of the rocket using segmental ballistic linearization methodology based on small turbulence theory. Based on the model, the application of linear adjoint method in rocket is studied. Ballistic error is deduced and analyzed. Finally the feasibility of applying linear adjoint method to rocket error is testified through computer simulation.",
keywords = "Adjoint method, Error analysis, Linearization, Rocket",
author = "Dunhui Zhao and Jiabin Chen and Jun Xu and Zhide Liu and Yongqiang Han",
year = "2009",
doi = "10.1109/PACIIA.2009.5406471",
language = "English",
isbn = "9781424446070",
series = "PACIIA 2009 - 2009 2nd Asia-Pacific Conference on Computational Intelligence and Industrial Applications",
pages = "146--149",
booktitle = "PACIIA 2009 - 2009 2nd Asia-Pacific Conference on Computational Intelligence and Industrial Applications",
note = "2009 2nd Asia-Pacific Conference on Computational Intelligence and Industrial Applications, PACIIA 2009 ; Conference date: 28-11-2009 Through 29-11-2009",
}