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ASME Press Select Proceedings

International Conference on Mechanical Engineering and Technology (ICMET-London 2011)

Editor
Garry Lee
Garry Lee
Information Engineering Research Institute
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ISBN:
9780791859896
No. of Pages:
906
Publisher:
ASME Press
Publication date:
2011

The impulse control model is given. The limitations of traditional genetic algorithm are considered. Combining with the characteristics of pulse vector controller ignition, an improved genetic algorithm is proposed, and the algorithm is suitable for pulse engine ignition model. The algorithm is used in the process of pulse vector controller optimization ignition. Simulation example shows that ignition control problem of the pulse vector controller can be solved effectively with this algorithm. Technical requirements which require missile system fast response, low energy consumption and high precision tracking can be reached.

Abstract
Keywords
Introduction
Impulse Control Model
Simulation
Conclusion
References
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