Quad-Rotor Aircraft Hovering Mode ITAE Optimal PID Control

ZHANG Tian-yi; ZHAO Qing-zhan; LIU Wei

doi:10.3969/j.issn.1671-637x.2016.08.011

Journals >Electronics Optics & Control >Volume 23 >Issue 8 >Page 48 > Article

Electronics Optics & Control
Vol. 23, Issue 8, 48 (2016)

Quad-Rotor Aircraft Hovering Mode ITAE Optimal PID Control

ZHANG Tian-yi^1、2, ZHAO Qing-zhan^2、3, and LIU Wei^3、4

Author Affiliations

¹[in Chinese]

²[in Chinese]

³[in Chinese]

⁴[in Chinese]

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DOI: 10.3969/j.issn.1671-637x.2016.08.011 Cite this Article

ZHANG Tian-yi, ZHAO Qing-zhan, LIU Wei. Quad-Rotor Aircraft Hovering Mode ITAE Optimal PID Control[J]. Electronics Optics & Control, 2016, 23(8): 48 Copy Citation Text

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References

[8] TAYEBI A, MCGILVRAY S. Attitude stabilization of a VTOL quadrotor aircraft［J］. IEEE Transactions on Control Systems Technology, 2006, 14(3): 562-571.

[10] SALIH A L, MOGHAVVEMI S M, HAF MOHAMED. Modelling and PID controller design for a quad-rotor unmannned air vehicle［C］//IEEE International Conference on Automuation, 2010, 1: 1-5.

CLP Journals

[1] FU Shaonan, YUAN Liang. An Image Moment Based Visual Servo Method for Quadrotor UAVs[J]. Electronics Optics & Control, 2020, 27(6): 71

ZHANG Tian-yi, ZHAO Qing-zhan, LIU Wei. Quad-Rotor Aircraft Hovering Mode ITAE Optimal PID Control[J]. Electronics Optics & Control, 2016, 23(8): 48

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