Xiucong Sun

According to our database, Xiucong Sun authored at least 11 papers between 2016 and 2025.

Collaborative distances:

• Dijkstra number of five.
• Erdős number of five.

2025

Skewed Unscented Kalman Filter Using Gaussian Sum.

Hanyu Liu, Xiucong Sun, Jinghao Yang, Ming Xu, Shengzhou Bai

IEEE Trans. Aerosp. Electron. Syst., April, 2025

Modified Unscented Kalman Filter Considering Maximum Point of Probability Density Function.

Hanyu Liu, Xiucong Sun, Shengzhou Bai

IEEE Trans. Aerosp. Electron. Syst., April, 2025

Two-Step Input Excitation Disturbance Estimation-Based Self-Adjustment Control for Spacecrafts With Multiplicative Uncertainties.

Yukai Zhu, Baopeng Zhu, Yangyang Cui, Xiucong Sun

IEEE Trans. Aerosp. Electron. Syst., February, 2025

Physics-Informed Data-Driven Autoregressive Nonlinear Filter.

Hanyu Liu, Xiucong Sun, Yuran Chen, Xinlong Wang

IEEE Signal Process. Lett., 2025

2023

Finite-Thrust Lambert Transfer Based on Multistage Constant-Vector Thrust Control.

Shengzhou Bai, Yuan Wang, Hanyu Liu, Xiucong Sun

IEEE Trans. Aerosp. Electron. Syst., October, 2023

2021

On the Feasibility of Orbit Determination From Gravity Gradient Invariants.

Xiucong Sun, Hao Zhang, Pei Chen, Chao Han

IEEE Trans. Aerosp. Electron. Syst., 2021

2017

Precise Real-Time Navigation of LEO Satellites Using a Single-Frequency GPS Receiver and Ultra-Rapid Ephemerides.

Xiucong Sun, Chao Han, Pei Chen

CoRR, 2017

2016

Autonomous orbit determination via kalman filtering of gravity gradients.

Xiucong Sun, Pei Chen, Christophe Macabiau, Chao Han

IEEE Trans. Aerosp. Electron. Syst., 2016

Low-Earth Orbit Determination from Gravity Gradient Measurements.

Xiucong Sun, Pei Chen, Christophe Macabiau, Chao Han

CoRR, 2016

Real-time kinematic positioning of LEO satellites using a single-frequency GPS receiver.

Pei Chen, Jian Zhang, Xiucong Sun

CoRR, 2016

Gravity Gradient Tensor Eigendecomposition for Spacecraft Positioning.

Pei Chen, Xiucong Sun, Chao Han

CoRR, 2016