TY - JOUR
T1 - A New Instantaneous Method for Attitude Determination Using GPS Phase Measurement
AU - Hsu, Tung Hsuan
AU - Chen, Tsung Lin
N1 - Publisher Copyright:
© 1963-2012 IEEE.
PY - 2022
Y1 - 2022
N2 - This article proposes a new algorithm for attitude determinations using GPS phase signals. The proposed method is an instantaneous method along with the small-angle assumption. Different from the existing methods, this method uses a newly defined performance index 'BDOP' to determine search sequences for different satellite signals, phase measurement noise, and baseline geometry to define the search space and ambiguity candidates' properties determined in previous search steps to reduce the search space for the subsequent searches. Consequently, the proposed method reduces the computation time and improves the attitude determination accuracy. The proposed method is verified both by numerical simulations and experiments. Simulation results indicate that the computation time of the proposed method is 0.01 s, the success rate 85%, and the angle estimation accuracy less than 1° when three antennas are installed 1 m apart, receiving GPS signals from five satellites, and the standard deviation of the phase measurement noise of 0.5 cm. In experiments, we verify the algorithms using a homemade three-antenna GPSR and a three-axis gimbal platform. The three antennas are installed 0.5 m apart and receive GPS signals from six satellites. The angle estimation error is less than 2° when the platform rotates in three axes simultaneously. In that experimental setup, the angle estimation degenerates at the large platform angles due to the signal interference from the ground effect and gimbal platform geometry.
AB - This article proposes a new algorithm for attitude determinations using GPS phase signals. The proposed method is an instantaneous method along with the small-angle assumption. Different from the existing methods, this method uses a newly defined performance index 'BDOP' to determine search sequences for different satellite signals, phase measurement noise, and baseline geometry to define the search space and ambiguity candidates' properties determined in previous search steps to reduce the search space for the subsequent searches. Consequently, the proposed method reduces the computation time and improves the attitude determination accuracy. The proposed method is verified both by numerical simulations and experiments. Simulation results indicate that the computation time of the proposed method is 0.01 s, the success rate 85%, and the angle estimation accuracy less than 1° when three antennas are installed 1 m apart, receiving GPS signals from five satellites, and the standard deviation of the phase measurement noise of 0.5 cm. In experiments, we verify the algorithms using a homemade three-antenna GPSR and a three-axis gimbal platform. The three antennas are installed 0.5 m apart and receive GPS signals from six satellites. The angle estimation error is less than 2° when the platform rotates in three axes simultaneously. In that experimental setup, the angle estimation degenerates at the large platform angles due to the signal interference from the ground effect and gimbal platform geometry.
KW - Attitude determinations
KW - carrier phase measurements
KW - instantaneous ambiguity resolution
KW - multiple antenna GPSR
UR - http://www.scopus.com/inward/record.url?scp=85122080781&partnerID=8YFLogxK
U2 - 10.1109/TIM.2021.3137158
DO - 10.1109/TIM.2021.3137158
M3 - Article
AN - SCOPUS:85122080781
SN - 0018-9456
VL - 71
JO - IEEE Transactions on Instrumentation and Measurement
JF - IEEE Transactions on Instrumentation and Measurement
ER -