@inproceedings{28287ceaba0243a2b55341027c91bd72,
title = "Study on homing guidance systems based on different source errors",
abstract = "To study the effect of heading error, angular noise and target glint on precision of missiles guidance, the PN, VP and BP guidance system models were established and base on the method of adjoints and non-dimensional method, the adjoint models of the three guidance systems were obtained and the expression of non-dimensional miss distance was deduced. It is concluded that the induced miss distance has a closely correlation with navigation constant N, system damping ratio and bandwidth while a low system damping ratio and bandwidth has bad influence on guidance precision. The miss distance does not decrease to zero but increase to a constant value with the increasing flight time of the engagement when angular noise and target glint is introduced. The miss distance of VP and BP guidance systems is lower than that of PN guidance system when only angular noise and target glint is introduced in the systems.",
keywords = "Angular noise, Body pursuit, Heading error, Method of adjoints, Miss distance, Proportional navigation, Target glint, Velocity pursuit",
author = "Hui Wang and Lin, \{De Fu\} and Jiang Wang and Cheng, \{Zhen Xuan\}",
year = "2010",
doi = "10.1109/CMCE.2010.5609891",
language = "English",
isbn = "9781424479566",
series = "2010 International Conference on Computer, Mechatronics, Control and Electronic Engineering, CMCE 2010",
pages = "118--121",
booktitle = "2010 International Conference on Computer, Mechatronics, Control and Electronic Engineering, CMCE 2010",
note = "2010 International Conference on Computer, Mechatronics, Control and Electronic Engineering, CMCE 2010 ; Conference date: 24-08-2010 Through 26-08-2010",
}