Interactive multiple model seeker filter for tracking evasive targets

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.

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    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)
    Division/Department: Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division
    Depositing User: Ms. Alphones Mary
    Date Deposited: 05 Mar 2009
    Last Modified: 07 Jul 2010 11:47
    URI: http://nal-ir.nal.res.in/id/eprint/5005

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