[HTML][HTML] Review of X-ray pulsar spacecraft autonomous navigation

W Yidi, W Zheng, S Zhang, GE Minyu… - Chinese Journal of …, 2023 - Elsevier
This article provides a review on X-ray pulsar-based navigation (XNAV). The review starts
with the basic concept of XNAV, and briefly introduces the past, present and future projects …

An adaptive anti-disturbance navigation method for polarized skylight-based autonomous integrated navigation system

Q Dou, T Du, Z Qiu, S Wang, J Yang - Measurement, 2022 - Elsevier
In satellite-denied confrontation or unstructured environments, the navigation performance
of the GPS will be severely restricted or even deceived. The SINS/polarization navigation …

Multi-cubesat relative position and attitude determination based on array signal detection in formation flying

J Wang, R Zhang, J Yuan, J Luo - IEEE transactions on …, 2019 - ieeexplore.ieee.org
High-precision relative position and attitude measurement is crucial for consensus control
and collision avoidance in multi-CubeSat formation flying. However, the traditional relative …

Derivative-free observability analysis of a stochastic dynamical system

Z Zheng, Y Xu, L Mili, Z Liu, L Peng… - IEEE Transactions on …, 2021 - ieeexplore.ieee.org
This paper proposes a novel approach to analyze the observability of a stochastic linear or
non-linear dynamical system. Unlike the traditional observability analysis approach, our …

Star angle modified with relativistic effects/StarNAV integrated navigation method for Mars exploration

M Gui, Y Wei, H Yang, Y Yang - Advances in Space Research, 2024 - Elsevier
The celestial navigation system based on star angle (SA) is a classical autonomous
navigation method for the spacecraft, which directly provides the position information of the …

A novel celestial aided time-differenced pulsar navigation method against ephemeris error of Jupiter for Jupiter exploration

M Gui, X Ning, X Ma, J Zhang - IEEE Sensors Journal, 2018 - ieeexplore.ieee.org
Subjected to the current observation technology, the planetary ephemerides which are used
to predict the positions of planets are not accurately known. For Jupiter exploration …

X-ray Pulsar Navigation Based on Phase and Doppler Frequency Shift Using Double-differenced

W Zhang, X Ma, X Chen, J Xu, X Sun… - IEEE Transactions on …, 2024 - ieeexplore.ieee.org
To suppress the systematic errors of the X-ray pulsar navigation system (XPNAV) based on
the phase and Doppler frequency shift, and eliminate singularity phenomena, a double …

A novel X-ray pulsar integrated navigation method for ballistic aircraft

Q Xu, H Wang, L Feng, S You, Y He - Optik, 2018 - Elsevier
Since X-ray pulsar navigation system (XNAV) has better anti-interference and autonomy, a
novel X-ray pulsar integrated navigation method combining celestial navigation system …

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 …

Methodology for state determination without prior information using x-ray pulsar navigation systems

K Lohan - 2021 - ideals.illinois.edu
Onboard measurements of periodic x-ray signals from highly stable, rapidly spinning stars
called pulsars, enable determination of spacecraft position, velocity, and attitude states. Due …