Non-singular Fast Terminal Sliding Mode Control of Attitude for Quad-rotor Aircrafts

LUO Lian-jie; DIAN Song-yi; PU Ming

doi:10.3969/j.issn.1671-637x.2018.04.003

Journals >Electronics Optics & Control >Volume 25 >Issue 4 >Page 12 > Article

Electronics Optics & Control
Vol. 25, Issue 4, 12 (2018)

Non-singular Fast Terminal Sliding Mode Control of Attitude for Quad-rotor Aircrafts

LUO Lian-jie¹, DIAN Song-yi¹, and PU Ming²

Author Affiliations

¹[in Chinese]

²[in Chinese]

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DOI: 10.3969/j.issn.1671-637x.2018.04.003 Cite this Article

LUO Lian-jie, DIAN Song-yi, PU Ming. Non-singular Fast Terminal Sliding Mode Control of Attitude for Quad-rotor Aircrafts[J]. Electronics Optics & Control, 2018, 25(4): 12 Copy Citation Text

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References

[1] ABDESSAMEUD ATAYEBI A.Global trajectory tracking control of VTOL-UAVs without linear velocity measurements［J］.Automatica201046(6):1053-1059.

[2] YANG K SCHENG C C.Robust adaptive controller design for a quadrotor helicopter［J］.Applied Mechanics & Materials2013284:2296-2300.

[3] DYDEK Z TANNASWAMY A MLAVRETSKY E.Adaptive control of quadrotor UAVs:a design trade study with flight evaluations［J］.IEEE Transactions on Control Systems Technology201321(4):1400-1406.

[4] XIONG J JZHENG E H.Position and attitude tracking control for a quadrotor UAV［J］.LSA Transactions2014 53(3):725-731.

[6] PATEL A RPATEL M AVYAS D R.Modeling and analysis of quadrotor using sliding mode control［C］//Proceeding of the 44th Southeastern Symposium on System Theory2012:111-114.

LUO Lian-jie, DIAN Song-yi, PU Ming. Non-singular Fast Terminal Sliding Mode Control of Attitude for Quad-rotor Aircrafts[J]. Electronics Optics & Control, 2018, 25(4): 12

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