Babu, KR and Sarma, IG and Swamy, KN (1995) Sliding mode estimation scheme for missile homing guidance. In: Automatic Control in Aerospace (Aerospace Control '94). A Postprint Volume from the IFAC Symposium, 12-16 Sept. 1994, Palo Alto, CA, USA, pp. 405-410.Full text not available from this repository.
A new approach to maneuvering target tracking using the Sliding Mode Observer theory, in the specific context of homing missile guidance, is developed. This scheme requires a priori information about the target acceleration bounds alone, and there is no need for a dynamic model to represent the target maneuver dynamics. The proposed estimator is as simple to implement as the conventional Extended Kalman Filter (EKF) itself. The simulation results, in the presence of realistic noise sources, demonstrate the superiority of the proposed estimation scheme over the EKF.
|Item Type:||Conference Paper|
|Additional Information:||Copyright of this article belongs to Pergamon.|
|Keywords:||aerospace control;missile guidance;state estimation;target tracking;variable structure systems|
|Department/Centre:||Division of Electrical Sciences > Computer Science & Automation (Formerly, School of Automation)|
|Date Deposited:||19 Sep 2007|
|Last Modified:||11 Jan 2012 05:49|
Actions (login required)