Application of a Single-Antenna GPS–Based Attitude Estimation on the Stability Control of a Small Unmanned Aerial Vehicle-Reference-Cited by-同舟云学术

Application of a Single-Antenna GPS–Based Attitude Estimation on the Stability Control of a Small Unmanned Aerial Vehicle

Published:2013-10 Issue:4 Volume:26 Page:768-785
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Ding Yi-Ren¹,Hsiao Fei-Bin²

Affiliation:

1. Ph.D. Student, Institute of Aeronautics and Astronautics, National Cheng Kung Univ., Taiwan 70101, ROC.

2. Distinguished Professor, Institute of Aeronautics and Astronautics, National Cheng Kung Univ., Taiwan 70101, ROC (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000204

Reference24 articles.

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2. Cho A. et al. (2007). “Fully automatic taxiing takeoff and landing of a UAV only with a single-antenna GPS receiver.” AIAA Infotech@Aerospace 2007 Conf. and Exhibit American Institute of Aeronautics and Astronautics Reston VA.

3. Cohen C. E. (1992). “Attitude determination using GPS.” Ph.D. thesis Dept. of Aeronautics and Astronautics Stanford Univ. Stanford CA.

4. Ding Y. R. Liu Y. C. Lin C. H. Tseng L. C. Teng Y. and Hsiao F. B. (2010). “The development of a small UAV with formation flight capability.” 25th Bristol Int. UAV Systems Conf. European Unmanned Systems Centre Rickmansworth U.K.

5. Euston M. Coote P. Mahony R. Kim J. and Hamel T. (2008). “A complementary filter for attitude estimation of a fixed-wing UAV.” IEEE/RSJ Int. Conf. on Intelligent Robots and Systems IEEE New York 340–345.

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