Stability Margin Clearance of Missile Autopilot Using μ Anylysis

Zhen Qian Hou; Xiao Geng Liang; Wen Zheng Wang; Qiang Feng Wang

doi:10.4028/www.scientific.net/AMM.198-199.995

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 198-199Stability Margin Clearance of Missile Autopilot...

Stability Margin Clearance of Missile Autopilot Using μ Anylysis

Abstract:

A new method of stability margin clearance of missile autopilot is described. First, a model of linear fractional transformation form is established for missile has uncertain parameters; then, the system stability margin requirements are seen as a virtual uncertainty and introduced into the model; Finally, the model is analyzed, and the clearance results about the missile autopilot performance is obtained. The results show this is a more efficient and accurate clearance method than traditional ones.

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Periodical:

Applied Mechanics and Materials (Volumes 198-199)

Pages:

995-1000

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.198-199.995

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Online since:

September 2012

Authors:

Zhen Qian Hou, Xiao Geng Liang, Wen Zheng Wang, Qiang Feng Wang

Keywords:

Autopilot, Clearance, Structured Singular Value

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References

[1] Christopher Fielding, Andras Varga, SamirBennani et al. Advanced Techniques for Clearance of Flight Control Laws[M]. Springer, (2002).

Google Scholar

[2] M. Herrnberger,M. Heller,S. Hecker et al. Advanced Uncertainty Modeling and Robustness Analysis for the Basic Flight Control System of a Modern Jet Trainer. AIAA Guidance, Navigation and Control Conference and Exhibit, (2007).

DOI: 10.2514/6.2007-6668

Google Scholar

[3] Karin Ståhl Gunnarsson, Jörgen Hansson, Fredrik Karlsson et al. Clearance of Flight Control Laws using Linear Fractional Transformations. AIAA Guidance, Navigation and Control Conference and Exhibit, (2004).

DOI: 10.2514/6.2004-4867

Google Scholar

[4] K. Glover, G. Vinnicombe, and G. Papageorgiou. Guaranteed multi-loop stabilitymargins and the gap metric. In 38th IEEE Conference on Decision and control, pages 4084-4085, 2000. Paper nunber 9007.

DOI: 10.1109/cdc.2000.912354

Google Scholar

[5] G. Vinnicombe. Measuring the Robustness of Feedback Systems. PhD thesis, University of Cambridge, (1993).

Google Scholar