Mechanical Analysis and Modeling for Tricopter

Yang Yang; Li Ling Xiang; Zhi Liu; Jin Feng Cui

doi:10.4028/www.scientific.net/AMM.455.304

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 455Mechanical Analysis and Modeling for Tricopter

Mechanical Analysis and Modeling for Tricopter

Abstract:

Distinguished quadrotor , the research of tricopter is still in undeveloped state. This paper focuses on torque analysis and mathematical modeling for attitude control of the tricopter aircraft. The simulation of controller shows that the PID method can not achieve the desired states, so the research of building the mathematical model provides some theoretical foundation for controlling the tricopter.

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Periodical:

Applied Mechanics and Materials (Volume 455)

Pages:

304-309

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.455.304

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Online since:

November 2013

Authors:

Yang Yang*, Li Ling Xiang, Zhi Liu, Jin Feng Cui

Keywords:

Flight Attitude, PID Control, Torque Analysis, Tricopter

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* - Corresponding Author

References

[1] LIU Lili . Research on the Modeling and Control to a Quadrotor Helicopter Simulator [D]. Zhong Nan University. (in Chinese).

Google Scholar

[2] LIU Huanye. Study and design of flight control systems for small scale quadrotor[D] . Shanghai Jiaotong University. (in Chinese).

Google Scholar

[3] WANG Shugang. Research of Quadrotor Control [D]. Harbin Institute of Technology. (in Chinese).

Google Scholar

[4] Sergio Salazar-Cruz, Real-Time Control of a Small-Scale Helicopter Having Three Rotors Compiègne, France{ssalazar, fkendoul, rlozano, ifantoni}[M].

Google Scholar

[5] S. Salazar-Cruz and R. Lozano. Stabilization and nonlinear control fora novel tri-rotor mini-aircraft, in proceedings of the IEEE ICRA'05, Barcelone, Spain, April 2005[C].

Google Scholar

[6] A. Tayebi, S. McGilvray, Attitude stabilization of a four-rotor aerial robot, IEEE Conference on Decision and Control, 2004[C].

DOI: 10.1109/cdc.2004.1430207

Google Scholar

[7] N. Guenard, T. Hamel, V. Moreau, Dynamic modeling and intuitive control strategy for an "X4-flyer, International Conference on Control and Automation, 2005[C].

DOI: 10.1109/icca.2005.1528106

Google Scholar

[8] S. Salazar-cruz, F. Kendoul, R. Lozano, I. Fantoni, Real-Time Stabilization of a Small Three-Rotor Aircraft, Aerospace and Electronic Systems Vol. 44, No. 2, 2008[C].

DOI: 10.1109/taes.2008.4560220

Google Scholar

[9] J. Escareno, A. Sanchez, O. Garcia, R. Lozano, Triple Tilting Rotor mini-UAV: Modeling and Embedded Control of the Attitude, American Control Conference, 2008[C].

DOI: 10.1109/acc.2008.4587031

Google Scholar