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By Yang Song, Yaqiong Chai, Fengrui Ye, Wenqiang Xu (auth.), Yinglin Wang, Tianrui Li (eds.)

ISBN-10: 3642256600

ISBN-13: 9783642256608

ISBN-10: 3642256619

ISBN-13: 9783642256615

"Proceedings of 2011 overseas convention on clever approach and data Engineering” offers chosen papers from the convention ISKE 2011, held December 15-17 in Shanghai, China. This court cases doesn’t purely research unique study and ways within the extensive parts of clever platforms and information engineering, but in addition current new methodologies and practices in clever computing paradigms. The booklet introduces the present medical and technical advances within the fields of synthetic intelligence, desktop studying, development attractiveness, information mining, info retrieval, knowledge-based platforms, wisdom illustration and reasoning, multi-agent platforms, natural-language processing, and so on. moreover, new computing methodologies are offered, together with cloud computing, provider computing and pervasive computing with conventional clever tools.
The lawsuits might be useful for either researchers and practitioners who are looking to make the most of clever equipment of their particular study fields.
Dr. Yinglin Wang is a professor on the division of laptop technological know-how and Engineering, Shanghai Jiao Tong college, China; Dr. Tianrui Li is a professor on the info technological know-how and expertise university, Southwest Jiaotong college, China; Dr. Da Ruan is a critical study scientist on the Belgian Nuclear learn Centre.

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Additional resources for Knowledge Engineering and Management: Proceedings of the Sixth International Conference on Intelligent Systems and Knowledge Engineering, Shanghai, China, Dec 2011 (ISKE2011)

Sample text

U= (22) If the guidance law and adaptive law are designed as the above equations, missile can hit the target in a uniform speed. The angle of LOS and acceleration can be stable.  ≈ 0 , so the final guidActually, in the process of terminal guidance, R ≈ R 0 , R ance law can be simplified by substituting these two equations. 4 Simulation In this section, a simulation comparison between the proposed guidance law and PNG in the vertical plane is presented. 4π t ) . During the terminal guidance, the velocity of target and missile are invariable.

It’s evident that they also result in the complexity in designing and analysis of the system simultaneously. Research on modern methods relative to guidance law is increasingly active. Lots of papers have been proposed in this research area. The optimal control theory has been used to develop the proportional navigation [5]. Sliding mode control method has been proposed applying in guidance of homing missile [6]. Using these methods, the integrated missile guidance and control system can be designed easily.

This paper is organized as follows. Design of the IEUC is presented in Section 2. Then, the IEUC algorithm is presented in Section 3. We apply the IEUC to a highspeed spinning process in Section 4. Finally, summary and concluding remarks are given in Section 5. 2 Design of the Immune-Enhanced Unfalsified Controller A novel immune-enhanced unfalsified controller (IEUC) is presented as shown in Fig. 1. The controller uses unfalsified control to evaluate preset candidate controllers and immune control to regulate control performance.

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Knowledge Engineering and Management: Proceedings of the Sixth International Conference on Intelligent Systems and Knowledge Engineering, Shanghai, China, Dec 2011 (ISKE2011) by Yang Song, Yaqiong Chai, Fengrui Ye, Wenqiang Xu (auth.), Yinglin Wang, Tianrui Li (eds.)


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