Advertisement
Published in:
2013 | OriginalPaper | Chapter
Cooperative Attack of Multiple Missiles Based on Optimal Guidance Law
Authors : Yuanqing Xia, Mengyin Fu
Published in: Compound Control Methodology for Flight Vehicles
Publisher: Springer Berlin Heidelberg
Activate our intelligent search to find suitable subject content or patents.
Select sections of text to find matching patents with Artificial Intelligence. powered by
Select sections of text to find additional relevant content using AI-assisted search. powered by
As is well known, the accurate guidance of a missile is a highly-concerned problem. Over these decades, persistent efforts have been made to meet the increasingly need for the accuracy of missile guidance. While there has been rapid improvement in realizing the physical conditions for high-speed missile guidance and intercepting missiles, various theories in this field are also created. Dated back to 30 years ago, Guelman [89] made a comprehensive study of PN, which is widely considered as a very significant and fundamental theory of missile guidance. Since then, PN guidance law has been complemented and extended. For example, Becker [19] obtained a closed form solution of PN. Ghawghawe et al.