Design and Analysis of Nonlinear Autopilot for Tactical Missile

Lei Wang; Zai Kang Qi

doi:10.4028/www.scientific.net/AMM.313-314.1139

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 313-314Design and Analysis of Nonlinear Autopilot for...

Design and Analysis of Nonlinear Autopilot for Tactical Missile

Abstract:

A compromise design approach for nonlinear autopilot for tactical missile is detailed from an application point of view. The nonlinear actuator is treated by description function. The damping loop and acceleration loop is dealt with using separation design strategy, respectively. The feasibility and correctness of this proposed method is validated by simulation results.

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Periodical:

Applied Mechanics and Materials (Volumes 313-314)

Pages:

1139-1143

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.313-314.1139

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Online since:

March 2013

Authors:

Lei Wang, Zai Kang Qi

Keywords:

Acceleration Loop, Damping Loop, Description Function, Nonlinear Autopilot

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References

[1] P. Zarchan. Tactical and strategic missile guidance [M]. 5th ed., AIAA, 2007.

Google Scholar

[2] Raziye Tekin, Özgür Ateşoğlu. Modeling and vertical launch analysis of an aero and thrust vector controlled surface to air missile [C]. AIAA Atmospheric Flight Mechanics Conference, Aug. 2010: 1-17.

DOI: 10.2514/6.2010-7639

Google Scholar

[3] C. P. Mracek, D. B. Ridgely. Missile longitudinal autopilots: connections between optimal control and classical topologies [C]. AIAA Guidance, Navigation and Control Conference and Exhibit, Aug. 2005: 1-29.

DOI: 10.2514/6.2005-6381

Google Scholar

[4] Song Zhen-duo. Demonstrate and test of anti-tank missile weapons [M]. Beijing: National Defense Industry Publishing Company, 2003.

Google Scholar

[5] Qi Zai-kang. Guided weapon control systems. Beijing Institute of Technology Press, 2003.

Google Scholar

[6] Qian Xing-fang, Lin Rui-xiong and Zhao Ya-nan. Missile flight dynamics. Beijing Institute of Technology Press, 2008. (in Chinese)

Google Scholar

[7] João P. Hespanha. Linear systems theory, Princeton University Press, 2009.

Google Scholar