State Space Analysis and Optimal Control for Aircraft Simulator Pitch Electric Control Loading System

Chun Ping Pan; Li Xin Li; Yong Liang Wang

doi:10.4028/www.scientific.net/AMM.367.382

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 367State Space Analysis and Optimal Control for...

State Space Analysis and Optimal Control for Aircraft Simulator Pitch Electric Control Loading System

Abstract:

An electric control loading system for aircraft simulation was analyzed and modeled to find a linear state space mathematical model and state feedback. An optimal control scheme based on the minimum integral of the squared difference between desired and actual output was shown to be effective by comparing the output values of the system with previously obtained experimental data. A linear state space mathematical model and state feedback appear to provide satisfactory means for controlling an electric control loading system can be adjusted to simulate a wide variety of real aircraft by altering input and output gains at the force analog computer when aircraft parameters are changed.

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Periodical:

Applied Mechanics and Materials (Volume 367)

Pages:

382-387

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.367.382

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Online since:

August 2013

Authors:

Chun Ping Pan, Li Xin Li, Yong Liang Wang

Keywords:

Aircraft Simulator, Electric Control Loading System, Optimal Control, State Feedback

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References

[1] LIU Yanwen, WANG Guangxiong, LI Jia. Passivity design for the control loading system of a flight simulator [J]. Acta Aeronautica et Astronautica Sinica, 2011, v32 (12): pp.2302-2309. (In Chinese).

Google Scholar

[2] QI Pan-guo, WANG Hui, HAN Jun-wei. Structured singular value-synthesis based robust control of hydraulic control loading system [J]. Journal of Jilin University (Engineering and Technology Edition) 2011, v. 41 (4): pp.1004-1009. (In Chinese).

Google Scholar

[3] ZHAO Jinsong, YE Zhengmao, SHEN Gang, HAN Junwei. Inverse Model Control for Inner Loop of control Loading System on Flight Simulator [J]. Journal of XI'AN Jiao Tong University. 2012, v46(4), pp.38-44. (In Chinese).

Google Scholar

[4] Mark Karpenko, Nariman Sepehri, Hardware-in-the-loop simulator for research on fault tolerant control of electro-hydraulic cylinders in a flight control application [J]. www. elsevier. com/ locate/mechatronics, 19 (2009), p.1067–1077.

DOI: 10.1016/j.mechatronics.2009.01.008

Google Scholar

[5] WANG Hui, XU Shoulin, FENG Yingjin, WANG Liwen. Testing Research for Control Loading System of Flight Simulator [J]. China mechanical engineering. 2008, v19 (14): pp.1720-1723. (In Chinese).

Google Scholar

[6] REN Changwei. Analysis and Design of Mechanism for Control Loading System of a Flight Simulator [D]. Harbin, Harbin Institute of Technology, 2010, pp.1-10. (In Chinese).

Google Scholar

[7] Information on http: /wenku. baidu. com/view/2f1169c189eb172ded63b747. html.

Google Scholar