Shantha Kumar, N and Kashyap, SK and Naidu, VPS and Girija, G (2008) Interactive multiple model seeker filter for tracking evasive targets. In: Proceedings of the International Conference on Aerospace Science and Technology (INCAST 2008-045), 26-28 Jun 2008, Bangalore, India.
![]() |
PDF
INCAST_2008-045.pdf Download (444kB) |
![]() |
Indexer Terms (Generate index codes conversion from application/pdf to indexcodes)
indexcodes.txt Download (4kB) |
Abstract
Seeker filter is an important subsystem in modern homing guidance system of advanced13; intercepting missiles. Seeker filter design for homing guidance requirements are highly demanding and13; challenging. Very low filter lag, high noise attenuation are some of the challenges that need to be addressed.13; This paper presents an interacting multiple model augmented extended Kalman filter (IMM-AEKF) design to13; operate as seeker filter in close loop homing guidance of an interceptor to track evasive targets. The13; performance of the seeker filter is verified with six degree of freedom interceptor-target engagement simulation13; with seeker filter in guidance loop of the interceptor. Different filter performance criteria have been used to13; verify the performance of the seeker filter. The seeker filter efficiently handles the various seeker noises and13; provides a smooth estimate of target states to generate guidance command for intercepting missile. The miss13; distance achieved is within the acceptable limits.
Item Type: | Conference or Workshop Item (Paper) |
---|---|
Additional Information: | Copyright for this article belongs to National Aerospace Laboratories |
Uncontrolled Keywords: | IMM-AEKF algorithm;Constant jerk (CJ) |
Subjects: | AERONAUTICS > Aeronautics (General) |
Depositing User: | Ms. Alphones Mary |
Date Deposited: | 05 Mar 2009 |
Last Modified: | 07 Jul 2010 06:17 |
URI: | http://nal-ir.nal.res.in/id/eprint/5005 |
Actions (login required)
![]() |
View Item |