[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 …

Maximum correntropy generalized high-degree cubature Kalman filter with application to the attitude determination system of missile

D Liu, X Chen, Y Xu, X Liu, C Shi - Aerospace Science and Technology, 2019 - Elsevier
For SINS/CNS integrated navigation system, the CKF can perform well for state estimation in
Gaussian noise. However, its performances are likely to degrade significantly under non …

Robust inertial navigation system/ultra wide band integrated indoor quadrotor localization employing adaptive interacting multiple model-unbiased finite impulse …

Y Xu, YS Shmaliy, X Chen, Y Li, W Ma - Aerospace Science and …, 2020 - Elsevier
A new adaptive interacting multiple model (IMM)-based unbiased finite impulse response
(UFIR)/Kalman filter (KF) algorithm is proposed to provide accurate and robust mini …

Dynamic estimation method for pulsar periods based on photon energy distribution folding and image template matching

TH Xie, X Ma, WJ Zhang, JR Li, ST Wang… - Astronomy & …, 2024 - aanda.org
Aims. The accuracy of the pulsar period estimation directly affects the restoration effect of the
signal profile. A more accurate pulsar profile will help improve the accuracy of pulsar delay …

Quantitative analysis of the carbon generation characteristics during Mg/CO2 combustion: Implications for suppressing carbon deposition

X Zhu, C Li, R Wei, W Ao, Y Guo, J Hu, J Yang… - Aerospace Science and …, 2020 - Elsevier
Carbon deposition can significantly reduce the working stability and specific impulse
performance of magnesium/carbon dioxide (Mg/CO 2) powder rocket engines; however, few …

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 …

Geometry error analysis in solar Doppler difference navigation for the capture phase

J Liu, XL Ning, X Ma, JC Fang - IEEE Transactions on …, 2019 - ieeexplore.ieee.org
Deep space exploration missions continue to become more ambitious, driving the need to
investigate autonomous navigation systems that are accurate and timely. The solar Doppler …

X-ray pulsar navigation based on two-stage estimation of Doppler frequency and phase delay

M Xue, D Peng, H Sun, H Shentu, Y Guo… - Aerospace Science and …, 2021 - Elsevier
In X-ray pulsar-based navigation (XPNAV), the appearance of Doppler effects caused by the
dynamic motion of the spacecraft would severely degrade the navigation accuracy. In this …

[HTML][HTML] A novel optimal data fusion algorithm and its application for the integrated navigation system of missile

LIU Di, C Xiyuan, LIU Xiao - Chinese Journal of Aeronautics, 2022 - Elsevier
Abstract For Inertial Navigation System (INS)/Celestial Navigation System (CNS)/Global
Navigation Satellite System (GNSS) integrated navigation system of the missile, the …

Heat-transfer characteristics of CO2 boiling flow in the regenerative cooling channel of an Mg/CO2 powder rocket engine for Mars missions

R Wei, C Hu, F Wu, J Hu, X Zhu, J Yang, F Li, C Li - Acta Astronautica, 2021 - Elsevier
To solve the problem of thermal protection posed by the long working time of Mg/CO 2
powder rocket engines, an experimental system is designed to study the heat-transfer …