@inproceedings{cb1d55885177475daecfd3a994f8c039,
title = "Research progress on design methods for missile integrated guidance and control",
abstract = "The design for missile integrated guidance control is to combine the missile guidance and control circuit into one loop. According to the relative motion of the missile and target, the control command is directly obtained to further improve the guidance and control precision. This paper summarizes the domestic and foreign research progress on the design methods of missile integrated guidance control in recent years, studies and summarizes its advantages and disadvantages, and analyzes the main problems and development trend of missile integrated guidance and control design.",
keywords = "Adaptive control, Control, Integrated guidance, Optimal control, Sliding mode control",
author = "Zhenhua Fu and Yaping Dai and Kuanqiao Zhang",
note = "Publisher Copyright: {\textcopyright} 2017 Association for Computing Machinery.; 2017 International Conference on Automation, Control and Robots, ICACR 2017 ; Conference date: 22-12-2017 Through 24-12-2017",
year = "2017",
month = dec,
day = "22",
doi = "10.1145/3175516.3175524",
language = "English",
series = "ACM International Conference Proceeding Series",
publisher = "Association for Computing Machinery",
pages = "15--19",
booktitle = "2017 International Conference on Automation, Control and Robots, ICACR 2017",
}