DocumentCode
2944603
Title
Real-time guidance of reusable winged space plane using genetic algorithm implemented on field programmable gate array
Author
Miyamoto, S. ; Narumi, T. ; Matsumoto, T. ; Yonemoto, K.
Author_Institution
Kyushu Inst. of Technol., Fukuoka, Japan
fYear
2012
fDate
11-14 July 2012
Firstpage
349
Lastpage
354
Abstract
An efficient and flexible real-time guidance system is one of the critical needs in the development of a future reusable space transportation system. The genetic algorithm employs an optimization model called the evolution of life, which is generally considered numerically robust but involves an extremely high calculation cost. To reduce the cost, this paper proposes an efficient procedure that optimizes the coefficients of a set of prescribed input functions. In addition, to reduce the calculation time by more than one tenth, the optimization scheme is implemented on a field programmable gate array. The resultant optimization system is applied to an on-board guidance system that optimizes the trajectory of an experimental winged rocket in real time.
Keywords
aerospace components; field programmable gate arrays; genetic algorithms; rockets; space vehicles; field programmable gate array; genetic algorithm; on-board guidance system; optimization model; real-time guidance; resultant optimization system; reusable space transportation system; reusable winged space plane; Computer aided software engineering; Erbium; Field programmable gate arrays; Genetic algorithms; Optimization; Rockets; Trajectory;
fLanguage
English
Publisher
ieee
Conference_Titel
Advanced Intelligent Mechatronics (AIM), 2012 IEEE/ASME International Conference on
Conference_Location
Kachsiung
ISSN
2159-6247
Print_ISBN
978-1-4673-2575-2
Type
conf
DOI
10.1109/AIM.2012.6266008
Filename
6266008
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