On Modeling and Control of Quadrotor Aircraft with Variable Blade Pitch

JIANG Hui-rong; DENG Zhi-cheng; ZHU Ming; PING Xue-shou

doi:10.3969/j.issn.1671-637x.2015.10.011

Journals >Electronics Optics & Control >Volume 22 >Issue 10 >Page 48 > Article

Electronics Optics & Control
Vol. 22, Issue 10, 48 (2015)

On Modeling and Control of Quadrotor Aircraft with Variable Blade Pitch

JIANG Hui-rong, DENG Zhi-cheng, ZHU Ming, and PING Xue-shou

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[in Chinese]

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DOI: 10.3969/j.issn.1671-637x.2015.10.011 Cite this Article

JIANG Hui-rong, DENG Zhi-cheng, ZHU Ming, PING Xue-shou. On Modeling and Control of Quadrotor Aircraft with Variable Blade Pitch[J]. Electronics Optics & Control, 2015, 22(10): 48 Copy Citation Text

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References

[1] SLOTINE J J E,LI W P.Applied nonlinear control［M］.Upper Saddle River,NJ: Prentice Hall,1990.

[2] SALIH A L,MOGHAVVEMI M,MOHAMED H A F,et al.Modelling and PID controller design for a quadrotor unmanned air vehicle［C］//Proceedings of the IEEE International Conference on Automation Quality and Testing Robotics,Cluj-Napoca,2010: 1-5.

JIANG Hui-rong, DENG Zhi-cheng, ZHU Ming, PING Xue-shou. On Modeling and Control of Quadrotor Aircraft with Variable Blade Pitch[J]. Electronics Optics & Control, 2015, 22(10): 48

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