@inproceedings{add82e87aaa94c158c8f62c6ccbca0d1,
title = "Finite-time convergent guidance and control based on integrated model",
abstract = "An integrated guidance and control model for missile control system design is established in this paper. Finite-time stability theory is used to design a finite-time convergent guidance and control law based on the proposed model. Some simulation tests are done to verify the validity of the control law designed in this paper and the advantages compared with other guidance laws. The results show the control designed in this paper can satisfy the terminal indicators accurately.",
keywords = "finite-time convergence control, terminal guidance, the integrated model",
author = "Lin Lin and Songyan Wang and Tao Chao and Ming Yang",
year = "2014",
doi = "10.1109/CCDC.2014.6852251",
language = "英语",
isbn = "9781479937066",
series = "26th Chinese Control and Decision Conference, CCDC 2014",
publisher = "IEEE Computer Society",
pages = "676--680",
booktitle = "26th Chinese Control and Decision Conference, CCDC 2014",
address = "美国",
note = "26th Chinese Control and Decision Conference, CCDC 2014 ; Conference date: 31-05-2014 Through 02-06-2014",
}