ePrints@IIScePrints@IISc Home | About | Browse | Latest Additions | Advanced Search | Contact | Help

Three dimensional PN based impact angle control for higher speed nonmaneuvering targets

Ghosh, Satadal and Ghose, Debasish and Raha, Soumyendu (2013) Three dimensional PN based impact angle control for higher speed nonmaneuvering targets. In: American Control Conference (ACC), 17-19 June 2013, Washington, DC, pp. 31-36.

[img] PDF
Ame_Cont_Conf_31_2013.pdf - Published Version
Restricted to Registered users only

Download (329Kb) | Request a copy
Official URL: http://ieeexplore.ieee.org/xpl/articleDetails.jsp?...

Abstract

Terminal impact angle control is crucial for enhancement of warhead effectiveness. In the literature, this problem has been addressed in the context of targets with lower speeds than the interceptor. However, in the current defence scenario, targets of much higher speed than the interceptor is a reality. This paper presents a generic proportional navigation (PN) based guidance law, that uses the standard PN and novel Retro-PN guidance laws based on the initial engagement geometry and terminal engagement requirements, for three dimensional engagement scenario against higher speed nonmaneuvering targets to control terminal impact angle. Results are obtained on the set of achievable impact angles and conditions on the navigation constant to achieve them. Simulation results are given to support the theoretical findings.

Item Type: Conference Paper
Related URLs:
Additional Information: Copyright of this article belongs to IEEE.
Department/Centre: Division of Information Sciences > Supercomputer Education & Research Centre
Division of Mechanical Sciences > Aerospace Engineering (Formerly, Aeronautical Engineering)
Date Deposited: 20 Dec 2013 08:59
Last Modified: 20 Dec 2013 08:59
URI: http://eprints.iisc.ernet.in/id/eprint/48076

Actions (login required)

View Item View Item