Combining dilution of precision and Kalman filtering for UWB positioning in a narrow space

Y Guo, W Li, G Yang, Z Jiao, J Yan - Remote Sensing, 2022 - mdpi.com
Affected by the spatial environment, the accuracy and stability of ultra-wideband (UWB)
positioning in a narrow space are significantly lower than those in the general indoor …

Enhanced GNSS-based positioning in space exploiting inter-spacecraft cooperation

A Delépaut, A Minetto, F Dovis, F Melman… - Proceedings of the 2022 …, 2022 - ion.org
The momentum taken by the space sector in the exploration of our Moon pushes private and
governmental actors to intensify their efforts for launching missions to our natural satellite. In …

Snapshot tracking of GNSS signals in space: A case study at lunar distances

A Nardin, A Minetto, S Guzzi, F Dovis, L Konitzer… - Proceedings of the 36th …, 2023 - ion.org
The latest space missions have unveiled GNSS usability for distances greater than 187 000
km from the Earth's surface. The actual availability and usability of GNSS signals beyond …

Intelligent navigation for the cruise phase of solar system boundary exploration based on Q-learning EKF

W Tao, J Zhang, H Hu, J Zhang, H Sun, Z Zeng… - Complex & Intelligent …, 2024 - Springer
With the continuous advancement of deep space exploration missions, the solar system
boundary exploration mission is established as one of the China's most important deep …

Variational Bayesian implicit unscented Kalman filter for celestial navigation using time delay measurement

M Gui, H Yang, X Ning, DJ Zhao, L Chen… - Advances in Space …, 2023 - Elsevier
Sunlight arrival time delay is an innovative measurement for celestial navigation, which
provides the distance information between the spacecraft and the nearby celestial body. For …

Formation of a satellite navigation system using X-ray pulsars

Z Hua, J Rong, X Luping - … of the Astronomical Society of the …, 2019 - iopscience.iop.org
The ephemeris of a pulsar is stable for a long time, which allows navigation based on pulsar
orientation to be vector feasible. The formation of a satellite navigation model using the …

Real-time and accurate pulsar time-of-arrival estimation using GA-optimized EMD-CS

L Liu, J Liu, X Ning, Z Kang - Optik, 2021 - Elsevier
For the estimation methods of the pulsar TOA (time-of-arrival) based on CS (compressed
sensing), it is very important to construct the measurement matrix, which affects accuracy …

Orbit determination using pulsar timing data and orientation vector

H Zhang, R Jiao, L Xu - The Journal of Navigation, 2019 - cambridge.org
X-ray Pulsar Navigation (XPNAV) uses the Time Difference of Arrival (TDOA) of the pulsar
signal between the spacecraft and Solar System Barycentre (SSB) to determine position. In …

X-ray pulsar-based GNC system for formation flying in high Earth orbits

J Song, C Pirat, V Gass, G Xu, Z Zhang, J Zhang - Acta Astronautica, 2020 - Elsevier
In this paper, comprehensive pulsar-based Guidance, Navigation and Control (GNC) system
is designed and applied to satellites formation flying. The complete autonomy of the X-ray …

On the feasibility of orbit determination from gravity gradient invariants

X Sun, H Zhang, P Chen, C Han - IEEE Transactions on …, 2020 - ieeexplore.ieee.org
The capability of full-tensor gravity gradients for spacecraft orbit determination has been
demonstrated in recent studies. The advantages lie in its independence from ground-based …