@inproceedings{ddfb7e48ffe24805a3165b50ecf347b2,
title = "Missile trajectory optimization using Steepest Ascent method",
abstract = "A Steepest Ascent numerical procedure for offline trajectory optimization of a surface-to-surface missile attacking a stationary target is presented. A detailed numerical solution, starting from building the mathematical formulation till generating an offline angle of attack control history is illustrated. The formulation entails nonlinear 2-dimensional missile flight dynamics with mixed boundary conditions. The influences of the optimization algorithm controlling parameters are investigated. A new weighting matrix is proposed. Finally, a comparison between the obtained control history and the one obtained by a nonlinear optimal control package 'GPOPS' is presented. The results indicate that the use of Steepest Ascent method, to a great extent, is comparable in accuracy and iteration time to the well known optimization package 'GPOPS'.",
keywords = "Steepest Ascent, influence functions, step response, trajectory optimization",
author = "Khalil, \{Elsayed M.\} and Zhou Hao and Wanchun Chen",
note = "Publisher Copyright: {\textcopyright} 2013 IEEE.; 2013 3rd International Conference on Computer Science and Network Technology, ICCSNT 2013 ; Conference date: 12-10-2013 Through 13-10-2013",
year = "2014",
month = nov,
day = "25",
doi = "10.1109/ICCSNT.2013.6967333",
language = "英语",
series = "Proceedings of 2013 3rd International Conference on Computer Science and Network Technology, ICCSNT 2013",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "1269--1275",
booktitle = "Proceedings of 2013 3rd International Conference on Computer Science and Network Technology, ICCSNT 2013",
address = "美国",
}