Geomagnetic Field Measurements based Adaptive Cubature H-infinity Filter for Microsatellite Autonomous Orbit Estimation

Z Li, X Yang, L Li, Y Liao - 2024 - preprints.org
To address the issue of reduced orbit estimation accuracy resulting from discrepancies
between in-orbit measured geomagnetic field values and IGRF model values in autonomous …

Guidepost-based autonomous orbit determination method for GEO satellite

B Hou, J Wang, H Zhou, Z He, D Li, X Liu - Advances in Space Research, 2021 - Elsevier
Guidepost-based navigation system is a novel autonomous orbit determination method for
the GEO satellite. The system is achieved by using the camera imaging function to obtain the …

Microsatellite autonomous orbit propagation method based on SGP4 model and GPS data

X Liu, B Yuan, Z Meng - 2018 IEEE CSAA Guidance, Navigation …, 2018 - ieeexplore.ieee.org
With the development of aerospace technology, it is possible nowadays to develop orbit
propagation algorithms for microsatellite autonomous flight. In recent years, global …

[HTML][HTML] Robust UKF orbit determination method with time-varying forgetting factor for angle/range-based integrated navigation system

Q QIANG, LIN Baojun, LIU Yingchun, LIN Xia… - Chinese Journal of …, 2024 - Elsevier
The angle/range-based integrated navigation system is a favorable navigation solution for
deep space explorers. However, the statistical characteristics of the measurement noise are …

Magnetometer-based autonomous orbit determination via a measurement differencing extended Kalman filter during geomagnetic storms

F Cui, D Gao, J Zheng - Aircraft Engineering and Aerospace …, 2020 - emerald.com
Purpose The main reason for the low accuracy of magnetometer-based autonomous orbit
determination is the coarse accuracy of the geomagnetic field model. Furthermore, the …

Precise orbit determination of low-Earth satellites: a comparison of batch and real-time filtering techniques

L FIORESE - thesis.unipd.it
Abstract Precise Orbit Determination (POD) has become more and more relevant over the
past decades due to the ever increasing requirements artificial satellites must satisfy. This is …

An efficient micro-satellite attitude estimation algorithm based on QUEST and UD-MEKF

M Yang, Y Chen, X Xin - 2021 33rd Chinese Control and …, 2021 - ieeexplore.ieee.org
This paper designed an efficient algorithm for attitude estimation using the information from
the sun sensors/magnetometers/Micro-Electro-Mechanical System (MEMS) gyroscopes. The …

Attitude and in-orbit residual magnetic moment estimation of small satellites using only magnetometer

R Srivastava, R Sah, K Das - arXiv preprint arXiv:2107.09257, 2021 - arxiv.org
Attitude estimation or determination is a fundamental task for satellites to remain effectively
operational. This task is furthermore complicated on small satellites by the limited space and …

Pico-satellite autonomous navigation with magnetometer and sun sensor data

H Ke, W Hao, TU Binjie, JIN Zhonghe - Chinese Journal of Aeronautics, 2011 - Elsevier
This article presents a near-Earth satellite orbit estimation method for pico-satellite
applications with light-weight and low-power requirements. The method provides orbit …

Improving extended Kalman filter algorithm in satellite autonomous navigation

L He, H Zhou, G Zhang - Proceedings of the Institution of …, 2017 - journals.sagepub.com
With the goal of reducing dependence on ground tracking systems, satellite autonomous
navigation technologies are developed quickly in the recent several decades. However …