Research on the Necessity of Lie Group Strapdown Inertial Integrated Navigation Error Model Based on Euler Angle. - Leiyuan Qian; Fangjun Qin; Kailong Li; Tiangao Zhu (Sensors, 2022)

Analysis of the Influence of Different Reference Models on Recovering Gravity Anomalies from Satellite Altimetry. - Yu Han; Fangjun Qin; Hongwei Wei; Fengshun Zhu; Leiyuan Qian (Remote. Sens., 2024)

High-Precision Atom Interferometer-Based Dynamic Gravimeter Measurement by Eliminating the Cross-Coupling Effect. - Yang Zhou; Wenzhang Wang; Guiguo Ge; Jinting Li; Danfang Zhang; Meng He 006; Biao Tang; Jiaqi Zhong; Lin Zhou; Runbing Li; Ning Mao; Hao Che; et al. (Sensors, 2024)

The Optimized SINS/DVL Integration Based on SE₃(3) Quaternion Error Model and Adaptive Estimator. - Leiyuan Qian; Lubin Chang; Kailong Li; Fangjun Qin; Tiangao Zhu; Penghua Gao (IEEE Trans. Instrum. Meas., 2025)

A Novel Error Model Based on Quaternion of Body Frame of SE(3) for Inertial-Integrated Navigation. - Tiangao Zhu; An Li; Kailong Li; Leiyuan Qian; Wenkui Li; Yongbing Chen (IEEE Trans. Instrum. Meas., 2025)