Integrated Navigation System for a Low-Cost Quadrotor Aerial Vehicle in the Presence of Rotor Influences

Author:

Zhou Zebo1,Li Yong2,Zhang Jianfeng3,Rizos Chris4

Affiliation:

1. Associate Professor, School of Aeronautics and Astronautics, Univ. of Electronic Science and Technology of China, Chengdu 611731, China; Visiting Fellow, State Key Laboratory of Geodesy and Earth's Dynamics, Institute of Geodesy and Geophysics Chinese Academy of Sciences, Wuhan 430077, China; Visiting Fellow, Surveying and Geospatial Engineering School of Civil and Environmental Engineering, Univ. of New South Wales, Sydney 2052, Australia (corresponding author).

2. Senior Research Fellow, Surveying and Geospatial Engineering, School of Civil and Environmental Engineering, Univ. of New South Wales, Sydney 2052, Australia.

3. Master’s Candidate, School of Aeronautics and Astronautics, Univ. of Electronic Science and Technology of China, Chengdu 611731, China.

4. Professor, Surveying and Geospatial Engineering, School of Civil and Environmental Engineering, Univ. of New South Wales, Sydney 2052, Australia.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Civil and Structural Engineering

Reference32 articles.

1. Achtelik M. Bachrach A. He R. Prentice S. and Roy N. (2009). “Autonomous navigation and exploration of a quadrotor helicopter in GPS-denied indoor environments.” Int. Aerial Robotics Competition First Symp. on Indoor Flight Issues AUVSI Mayaguez Puerto Rico.

2. Allan D. W. (1966). “Statistics of atomic frequency standards.” Proc. IEEE 54(2) 221–230. 10.1109/PROC.1966.4634

3. Altug E. Ostrowski J. P. and Mahony R. (2002). “Control of a quadrotor helicopter using visual feedback.” Proc. IEEE Int. Conf. on Robotics and Automation IEEE New York 72–77.

4. Bak T. (2001). “Vision-GPS fusion for guidance of an autonomous vehicle in row crops.” Proc. 14th Int. Technical Meeting of the Satellite Div. of the Institute of Navigation (ION GPS 2001) Institute of Navigation Manassas VA 423–429.

5. Autonomous Vehicle Technologies for Small Fixed-Wing UAVs

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