Ghose, D and Dam, B and Prasad, UR (1989) A Spread Acceleration Guidance Scheme for Command Guided Surface-To-Air Missiles. In: IEEE 1989 National Aerospace and Electronics Conference. NAECON 1989, 22-26 May, Dayton,OH, Vol.1, 202-208.
A new guidance law for command guided surface-to-air missiles is presented. It attempts to reduce the integral control effort while at the same time takes into account the maneuvers of the target. A Monte-Carlo simulation of a missile-target engagement in an inclined plane is carried out to check the performance of the new guidance law in comparison with existing laws in terms of integral control effort, interception time and miss distance.
|Item Type:||Conference Paper|
|Additional Information:||Copyright 1989 IEEE. Personal use of this material is permitted. However, permission to reprint/republish this material for advertising or promotional purposes or for creating new collective works for resale or redistribution to servers or lists, or to reuse any copyrighted component of this work in other works must be obtained from the IEEE.|
|Department/Centre:||Division of Electrical Sciences > Electrical Engineering
Division of Electrical Sciences > Electrical Communication Engineering
Division of Electrical Sciences > Computer Science & Automation (Formerly, School of Automation)
|Date Deposited:||31 May 2006|
|Last Modified:||19 Sep 2010 04:28|
Actions (login required)