DocumentCode :
724375
Title :
Review of studies on integrated guidance and control design approach
Author :
Xiangyu Sun ; Tao Chao ; Songyan Wang ; Ming Yang
Author_Institution :
Control & Simulation Centre, Harbin Inst. of Technol., Harbin, China
fYear :
2015
fDate :
23-25 May 2015
Firstpage :
3958
Lastpage :
3963
Abstract :
Ending game of vehicle has properties of nonlinearity and quick states variation. To solve these problems, a newly developing approach that integrated guidance and control design attracts attention. This article firstly introduces research significance and design direction of the approach, and then divides the development procedure into several research phases meanwhile summarizes the results of each one. This approach solves numerous problems in traditional separate design approach and reduces design cost. Through the analysis of the current research situation combined with the actual demand, many key problems still need to be solved in future. Some prospects about this design approach are shown at last.
Keywords :
control nonlinearities; control system synthesis; missile guidance; hypersonic vehicle ending game; integrated guidance and control design; nonlinearity; precision guided weapons; Finite-time; Integrated guidance and control; Nonlinear;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control and Decision Conference (CCDC), 2015 27th Chinese
Conference_Location :
Qingdao
Print_ISBN :
978-1-4799-7016-2
Type :
conf
DOI :
10.1109/CCDC.2015.7162615
Filename :
7162615
Link To Document :
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