Sarkar, AK and Ananthasayanam, MR and Srinivasan, T and Kar, PK (2009) Comparison of the Radar and Seeker Modes of Pursuer Guidance. In: Journal of guidance control and dynamics, 32 (6). pp. 1912-1920.
PDF
AIAA-40404-599.pdf - Published Version Restricted to Registered users only Download (1MB) | Request a copy |
Abstract
This paper compares closed-loop performance of seeker-based and radar-based estimators for surface-to-air interception through 6-degree-of-freedom simulation using proportional navigation guidance.Ground radar measurements are evader range, azimuth and elevation angles contaminated by Gaussian noise. Onboard seeker measurements are pursuer-evader relative range, range rate also contaminated by Gaussian noise. The gimbal angles and line-of-sight rates in the gimbal frame,contaminated by time-correlated non-Gaussian noise with realistic numerical values are also available as measurements. In both the applications, extended Kalman filter with Gaussian noise assumption are used for state estimation. For a typical engagement, it is found that,based on Monte Carlo studies, seeker estimator outperforms radar estimator in terms of autopilot demand and reduces the miss distance.Thus, a seeker estimator with white Gaussian assumption is found to be adequate to handle the measurements even in the presence of non-Gaussian correlated noise. This paper uses realistic numerical values of all noise parameters.
Item Type: | Journal Article |
---|---|
Publication: | Journal of guidance control and dynamics |
Publisher: | American Institute of Aeronautics and Astronautics |
Additional Information: | copyright of this article belongs to American Institute of Aeronautics and Astronautics. |
Department/Centre: | Division of Mechanical Sciences > Aerospace Engineering(Formerly Aeronautical Engineering) |
Date Deposited: | 10 Jan 2010 11:59 |
Last Modified: | 19 Sep 2010 05:53 |
URI: | http://eprints.iisc.ac.in/id/eprint/25282 |
Actions (login required)
View Item |