DocumentCode
3364348
Title
Maximum Range computation based on differential flatness for guided bombs
Author
Geng, Lina ; Sun, Weimeng ; Zheng, Zhiqiang
Author_Institution
Coll. of Mechatron. Eng. & Autom., Nat. Univ. of Defense Technol., Changsha, China
fYear
2009
fDate
9-12 Aug. 2009
Firstpage
2026
Lastpage
2030
Abstract
The paper presents an efficient computational method for Maximum Range of guided bombs based on differential flatness. Differential flatness theory is briefly described and original motion model of guided bomb is reformulated by introducing flat outputs. The original states and inputs can be defined in terms of the flat outputs and their derivatives, and all the boundary conditions and path constraints are also mapped into the flat output space. Any curve that satisfies the boundary conditions as well as path constraints is a solution trajectory of the original system. Therefore, maximum range trajectory is planned in the flat output space. Then, the dynamic optimization problem is translated into static optimization one by collocation method. Finally, the computation approach is proved to be feasible and optimal by an initial trajectory integral that the target is set at maximum range.
Keywords
missile guidance; position control; boundary conditions; collocation method; differential flatness; dynamic optimization problem; guided bombs; initial trajectory integral; maximum range computation; path constraints; static optimization; Automation; Boundary conditions; Costs; Differential equations; Mathematical model; Optimal control; Optimization methods; Performance analysis; Polynomials; Weapons; collocation method; constrained trajectory; differential flatness; guided bomb;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronics and Automation, 2009. ICMA 2009. International Conference on
Conference_Location
Changchun
Print_ISBN
978-1-4244-2692-8
Electronic_ISBN
978-1-4244-2693-5
Type
conf
DOI
10.1109/ICMA.2009.5246267
Filename
5246267
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