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State estimation of spiralling target using UKF with generalized sinusoidal target acceleration model

Dwivedi, PN and Bhale, PG and Bhattacharya, A and Padhi, R (2012) State estimation of spiralling target using UKF with generalized sinusoidal target acceleration model. In: AIAA Guidance, Navigation, and Control Conference, 13-16 August 2012, Minneapolis, Minnesota.

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Official URL: http://dx.doi.org/10.2514/6.2012-4891

Abstract

Hit-to-kill interception of high velocity spiraling target requires accurate state estimation of relative kinematic parameters describing spiralling motion. In this pa- per, spiraling target motion is captured by representing target acceleration through sinusoidal function in inertial frame. A nine state unscented Kalman filter (UKF) formulation is presented here with three relative positions, three relative velocities, spiraling frequency of target, inverse of ballistic coefficient and maneuvering coef-ficient. A key advantage of the target model presented here is that it is of generic nature and can capture spiraling as well as pure ballistic motions without any change of tuning parameters. Extensive Six-DOF simulation experiments, which includes a modified PN guidance and dynamic inversion based autopilot, show that near Hit-to-Kill performance can be obtained with noisy RF seeker measurements of gimbal angles, gimbal angle rates, range and range rate.

Item Type: Conference Paper
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Additional Information: Copyright of this article belongs to AIAA American Institute of Aeronautics and Astronautics.
Department/Centre: Division of Mechanical Sciences > Aerospace Engineering (Formerly, Aeronautical Engineering)
Date Deposited: 04 Mar 2014 11:32
Last Modified: 04 Mar 2014 11:32
URI: http://eprints.iisc.ernet.in/id/eprint/48530

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