Attitude Estimation for Quad-Rotor Aircraft

RAO Kang-qi; LIU Xiao-ming; CHEN Wan-chun

doi:10.3969/j.issn.1671-637x.2015.05.006

Journals >Electronics Optics & Control >Volume 22 >Issue 5 >Page 25 > Article

Electronics Optics & Control
Vol. 22, Issue 5, 25 (2015)

Attitude Estimation for Quad-Rotor Aircraft

RAO Kang-qi, LIU Xiao-ming, and CHEN Wan-chun

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[in Chinese]

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DOI: 10.3969/j.issn.1671-637x.2015.05.006 Cite this Article

RAO Kang-qi, LIU Xiao-ming, CHEN Wan-chun. Attitude Estimation for Quad-Rotor Aircraft[J]. Electronics Optics & Control, 2015, 22(5): 25 Copy Citation Text

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References

[1] BAERVELDT A J, KLANG R.A low-cost and low-weight attitude estimation system for an autonomous helicopter［C］//International Conference on Intelligent Engineering Systems, 1997: 391-395.

[2] HOFFMANN F, GODDEMEIER N, BERTRAM T.Attitude estimation and control of a quadrocopter［C］//IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS), Taipei: IEEE, 2010: 1072-1077.

RAO Kang-qi, LIU Xiao-ming, CHEN Wan-chun. Attitude Estimation for Quad-Rotor Aircraft[J]. Electronics Optics & Control, 2015, 22(5): 25

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