A Three-Dimensional Cooperative Guidance Law of Multimissile System. (4th October 2015)

• Record Type: Journal Article
• Authors: Wei, Xing; Wang, Yongji; Dong, Shuai; Liu, Lei
• Other Names: Damaren Christopher J. Academic Editor.
• Is Part Of: International journal of aerospace engineering. Volume 2015(2015)
• Publication Date: 2015-10-04
• Subjects: Aerospace engineering -- Periodicals; 629.105
• DOI: 10.1155/2015/479427
• Languages: English
• ISSNs: 1687-5966

Abstract

Abstract : In order to conduct saturation attacks on a static target, the cooperative guidance problem of multimissile system is researched. A three-dimensional guidance model is built using vector calculation and the classic proportional navigation guidance (PNG) law is extended to three dimensions. Based on this guidance law, a distributed cooperative guidance strategy is proposed and a consensus protocol is designed to coordinate the time-to-go commands of all missiles. Then an expert system, which contains two extreme learning machines (ELM), is developed to regulate the local proportional coefficient of each missile according to the command. All missiles can arrive at the target simultaneously under the assumption that the multimissile network is connected. A simulation scenario is given to demonstrate the validity of the proposed method.