NDLI: Circumnavigation control design of space flight vehicle using bearing measurement only

Content Provider	IEEE Xplore Digital Library
Author	Shen Yangfan He Fenghua Yi Fang Ma Longbiao
Copyright Year	2014
Description	Author affiliation: Control & Simulation Centre, Harbin Inst. of Technol., Harbin, China (Shen Yangfan; He Fenghua; Yi Fang; Ma Longbiao)
Abstract	The fly-around guidance control problem for non-cooperative target in orbital space is studied in this paper, in which only the relative angle measurement information and the space flight vehicle own motion information are available. We first established the mathematical model of the fly-around problem to describe the relative motion between a flight vehicle and its target, and the circumnavigation control problem is formulated as a math problem. Then, we design a control law of fly-around process and the convergence of the control law is also proved. Finally, the effectiveness of the proposed circumnavigation control design law is shown by some numerical simulation results.
Starting Page	602
Ending Page	607
File Size	977302
Page Count	6
File Format	PDF
ISBN	9789881563873
ISSN	19341768
DOI	10.1109/ChiCC.2014.6896693
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	Space vehicles non-cooperative target Control design Aerospace electronics control law of fly-around Extraterrestrial measurements space vehicle Electronic mail Mathematical model fly-around maneuver
Content Type	Text
Resource Type	Article

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