NDLI: Analysis and modeling of terminal guidance system for a flight vehicle with side-window detection

Content Provider	IEEE Xplore Digital Library
Author	Yang Baoqing Zheng Tianyu Zhang Silun Yao Yu
Copyright Year	2014
Description	Author affiliation: Harbin Inst. of Technol., Harbin, China (Yang Baoqing; Zheng Tianyu; Zhang Silun; Yao Yu)
Abstract	In this paper, the terminal guidance system of a flight vehicle with side-window detection is analyzed and modeled, in which the vision constraints caused by the side-window are considered. First, the most suitable encounter mode under different situations is given, by analyzing four possible engagement manners. Then, the convergence equivalence between LOS rate and body-LOS rate is proved since it is convenient to describe the side-window constraints in a body-LOS coordinate system. Then, the terminal guidance system of the flight vehicle is modeled in a body-LOS coordinate system in which the side-window constraints are converted into the constraints on states. The model combined with the attitude dynamics can be used in the on-going integrated design for the flight vehicle with side-window detection.
Starting Page	1051
Ending Page	1056
File Size	2308716
Page Count	6
File Format	PDF
ISBN	9789881563873
ISSN	19341768
DOI	10.1109/ChiCC.2014.6896773
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2014-07-28
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	TCCT, CAA
Subject Keyword	Terminal guidance system Analytical models Vision constraints Heating Aerodynamics Mathematical model Equations Vehicles Convergence Side-window detection
Content Type	Text
Resource Type	Article

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