Gravity Gradient Tensor Eigendecomposition for Spacecraft Positioning. - Pei Chen; Xiucong Sun; Chao Han 001 (CoRR, 2016)

Real-time kinematic positioning of LEO satellites using a single-frequency GPS receiver. - Pei Chen; Jian Zhang; Xiucong Sun (CoRR, 2016)

Low-Earth Orbit Determination from Gravity Gradient Measurements. - Xiucong Sun; Pei Chen; Christophe Macabiau; Chao Han 001 (CoRR, 2016)

Autonomous orbit determination via kalman filtering of gravity gradients. - Xiucong Sun; Pei Chen; Christophe Macabiau; Chao Han 001 (IEEE Trans. Aerosp. Electron. Syst., 2016)

Precise Real-Time Navigation of LEO Satellites Using a Single-Frequency GPS Receiver and Ultra-Rapid Ephemerides. - Xiucong Sun; Chao Han 001; Pei Chen (CoRR, 2017)

On the Feasibility of Orbit Determination From Gravity Gradient Invariants. - Xiucong Sun; Hao Zhang 040; Pei Chen; Chao Han 001 (IEEE Trans. Aerosp. Electron. Syst., 2021)

Finite-Thrust Lambert Transfer Based on Multistage Constant-Vector Thrust Control. - Shengzhou Bai; Yuan Wang; Hanyu Liu; Xiucong Sun (IEEE Trans. Aerosp. Electron. Syst., 2023)

Physics-Informed Data-Driven Autoregressive Nonlinear Filter. - Hanyu Liu; Xiucong Sun; Yuran Chen; Xinlong Wang (IEEE Signal Process. Lett., 2025)

Two-Step Input Excitation Disturbance Estimation-Based Self-Adjustment Control for Spacecrafts With Multiplicative Uncertainties. - Yukai Zhu 001; Baopeng Zhu; Yangyang Cui; Xiucong Sun (IEEE Trans. Aerosp. Electron. Syst., 2025)

Modified Unscented Kalman Filter Considering Maximum Point of Probability Density Function. - Hanyu Liu; Xiucong Sun; Shengzhou Bai (IEEE Trans. Aerosp. Electron. Syst., 2025)

Skewed Unscented Kalman Filter Using Gaussian Sum. - Hanyu Liu; Xiucong Sun; Jinghao Yang; Ming Xu 003; Shengzhou Bai (IEEE Trans. Aerosp. Electron. Syst., 2025)