NDLI: Relative impact angle control guidance law to intercept maneuvering target

Content Provider	IEEE Xplore Digital Library
Author	Hyun-Seung Kim Sang-Sup Park Chang-Kyung Ryoo
Copyright Year	2015
Description	Author affiliation: Dept. of Aerosp. Eng., Inha Univ., Incheon, South Korea (Hyun-Seung Kim; Sang-Sup Park; Chang-Kyung Ryoo)
Abstract	In this paper, a guidance law with a specified relative flight path angle constraint to intercept a highly maneuvering target is proposed. The RIAC(Relative Impact Angle Control) guidance law is used to enhance the target acquisition and tracking ability of seekers because the relative impact angle decides how clearly the target can be seen by the seeker. The proposed RIAC guidance law is modified from the well-known optimal IAC(Impact Angle Control) guidance law for a non-maneuvering target. By introducing relative impact angle and LOS(Line of Sight) rate into the IAC guidance law, the RIAC guidance law has the form of a biased pure PN(Proportional Navigation) guidance law with the terms of the conventional pure PN and the relative impact angle compensation. The performance of the proposed law was examined using full nonlinear 6-DOF simulations for anti-air missiles against ballistic targets.
Starting Page	836
Ending Page	841
File Size	732975
Page Count	6
File Format	PDF
ISBN	9784907764487
DOI	10.1109/SICE.2015.7285528
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2015-07-28
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	The Society of Instrument and Control Engineers - SICE
Subject Keyword	Missiles Navigation Trajectory Target tracking Optimal control Numerical simulation History Navigation Constant Impact Angle Control Biased Proportional Navigation Maneuvering Target Relative Flight Path Angle
Content Type	Text
Resource Type	Article

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