Event-triggered adaptive terminal sliding mode tracking control for drag-free spacecraft inner-formation with full state constraints

E Wang, S Qiu, M Liu, X Cao - Aerospace Science and Technology, 2022 - Elsevier
This paper investigates the reconstruction and maintenance of the inner-formation system
for an innovative drag-free spacecraft with double spherical test masses in consideration of …

[HTML][HTML] A review on DFACS (II): Modeling and analysis of disturbances and noises

YUE Chenglei, J Bohan, D Zhaohui… - Chinese Journal of …, 2024 - Elsevier
This paper presents Part II of a review on DFACS, which specifically focuses on the
modeling and analysis of disturbances and noises in DFACSs. In Part I, the system …

Underactuated spacecraft formation reconfiguration with collision avoidance

X Huang, Y Yan, Y Zhou - Acta astronautica, 2017 - Elsevier
Underactuated collision-free controllers are proposed in this paper for multiple spacecraft
formation reconfiguration in circular orbits with the loss of either the radial or in-track thrust. A …

The determination for ideal release point of test masses in drag-free satellites for the detection of gravitational waves

X Lian, J Zhang, J Yang, Z Lu, Y Zhang… - Advances in Space …, 2021 - Elsevier
Gravitational waves are ripples in space–time predicted by Albert Einstein's general relativity
and provide a new way to understand the universe. Space-borne detectors of gravitational …

Sliding mode control for Lorentz-augmented spacecraft hovering around elliptic orbits

X Huang, Y Yan, Y Zhou, H Zhang - Acta Astronautica, 2014 - Elsevier
A Lorentz spacecraft is an electrostatically charged space vehicle that could actively
modulate its surface charge to generate Lorentz force as it moves through the planetary …

Control design and analysis of an inner-formation flying system

Z Dang, Y Zhang - IEEE Transactions on Aerospace and …, 2015 - ieeexplore.ieee.org
Modeling of the dynamics and disturbances and designing of the precise formation
controller are two major problems for the inner-formation flying system (IFFS). This paper …

Optimal Lorentz-augmented spacecraft formation flying in elliptic orbits

X Huang, Y Yan, Y Zhou - Acta Astronautica, 2015 - Elsevier
An electrostatically charged spacecraft accelerates as it moves through the Earth׳ s
magnetic field due to the induced Lorentz force, providing a new means of propellantless …

Q-SAT for atmosphere and gravity field detection: Design, mission and preliminary results

W Zhaokui, H Dapeng, L Boxin, H Yunhan, Z Qi… - Acta Astronautica, 2022 - Elsevier
Q-SAT, a small spherical satellite designed and developed by Tsinghua university, was
successfully launched on Aug 6, 2020 at Jiuquan satellite launch center in China. The …

A spherical micro satellite design and detection method for upper atmospheric density estimation

Z Zhao, Z Wang, Y Zhang - International Journal of Aerospace …, 2019 - Wiley Online Library
A spherical microsatellite, aimed at technology verification of upper atmospheric density
detection and precision orbit determination in low Earth orbit (LEO), has been developed by …

Event‐triggered prescribed performance robust collision‐free capturing control for drag‐free spacecraft system

E Wang, M Liu, S Qiu, Y Yu… - IET Control Theory & …, 2022 - Wiley Online Library
This paper addresses the capturing control problem of a plug‐and‐play modularized drag‐
free spacecraft system, including two spherical proof masses, where the performance …