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