TY - GEN
T1 - Attitude and Position Estimation of Quad-rotor UAVs Through Computer-based Visualization
AU - He, Mo
AU - Cui, Naigang
N1 - Publisher Copyright:
© 2018 IEEE.
PY - 2018/8
Y1 - 2018/8
N2 - This paper presents a method that employs computer-visualization techniques for attitude and position estimation of quad-rotor unmanned aerial vehicles (UAVs). The proposed method employs minimal equipment-two digital cameras installed at the ground station and targets marked on the UAV body in the form of colored dots. An algorithm has been developed in the proposed study to recognize target dots in the images obtained from the two cameras, and hence, provide a match between them. The 3-D position of the target UAV and its attitude are then computed based on results of the matching exercise performed by the proposed algorithm. Different methods are employed to eliminate any incorrectly matched pair of images. Results of the experiment performed on the author's test bed demonstrate that the proposed method for attitude and position estimation attains high precision with translational and rotational errors of 5 cm and 3 degs, respectively, which are acceptable in most applications.
AB - This paper presents a method that employs computer-visualization techniques for attitude and position estimation of quad-rotor unmanned aerial vehicles (UAVs). The proposed method employs minimal equipment-two digital cameras installed at the ground station and targets marked on the UAV body in the form of colored dots. An algorithm has been developed in the proposed study to recognize target dots in the images obtained from the two cameras, and hence, provide a match between them. The 3-D position of the target UAV and its attitude are then computed based on results of the matching exercise performed by the proposed algorithm. Different methods are employed to eliminate any incorrectly matched pair of images. Results of the experiment performed on the author's test bed demonstrate that the proposed method for attitude and position estimation attains high precision with translational and rotational errors of 5 cm and 3 degs, respectively, which are acceptable in most applications.
UR - https://www.scopus.com/pages/publications/85082458979
U2 - 10.1109/GNCC42960.2018.9018933
DO - 10.1109/GNCC42960.2018.9018933
M3 - 会议稿件
AN - SCOPUS:85082458979
T3 - 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
BT - 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
Y2 - 10 August 2018 through 12 August 2018
ER -