NDLI: Guidance law design for air-to-surface missile to attack low velocity target

Content Provider	IEEE Xplore Digital Library
Author	Chen Peng Sentang Wu
Copyright Year	2008
Description	Author affiliation: Sch. of Autom. Sci. & Electr. Eng., Beijing Unversity of Aeronaut. & Astronaut., Beijing (Chen Peng; Sentang Wu)
Abstract	A new terminal guidance law is developed for a class of air-to-surface missiles to attack low velocity target on ground in this paper. The traditional proportional guidance law based on the angle rate of line-of-sight (LOS) is not proper for this attack problem because the angle rate of LOS is usually too small to be measured accurately. To resolve this problem, we present a new guidance law based on the angle of LOS only. The special characteristics of the terminal trajectory of this class of missiles are taken into account in the proposed guidance law. The full trajectory simulation results and analysis based on anti-ship missile are provided to demonstrate the effectiveness and accuracy of the proposed terminal guidance law.
Starting Page	3646
Ending Page	3649
File Size	255002
Page Count	4
File Format	PDF
ISBN	9781424417339
DOI	10.1109/CCDC.2008.4598010
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2008-07-02
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Missiles Terminal guidance Line-of-sight angle guidance Low velocity target Air-to-surface missile
Content Type	Text
Resource Type	Article

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Guidance law design for air-to-surface missile to attack low velocity target