Calculating collision probability for long-term satellite encounters through the reachable domain method
C Wen, D Qiao - Astrodynamics, 2022 - Springer
Satellite encounters during close operations, such as rendezvous, formation, and cluster
flights, are typical long-term encounters. The collision probability in such an encounter is a …
flights, are typical long-term encounters. The collision probability in such an encounter is a …
Finite-time distributed hierarchical control for satellite cluster with collision avoidance
S Li, C Liu, Z Sun - Aerospace Science and Technology, 2021 - Elsevier
In this paper, a novel distributed hierarchical control method for small satellites with multiple
disturbances and input constraints is investigated by combining formation flying and satellite …
disturbances and input constraints is investigated by combining formation flying and satellite …
Cooperative orbital control of multiple satellites via consensus
In space systems consisting of a large number of satellites, coordinating orbits among
satellites is necessary throughout the entire mission lifetime. Although previous works …
satellites is necessary throughout the entire mission lifetime. Although previous works …
A high thrust density voice coil actuator with a new structure of double magnetic circuits for cubesat deployers
Y Zhao, H Yue, F Yang, J Zhu - IEEE Transactions on Industrial …, 2021 - ieeexplore.ieee.org
The deployer uses a voice coil actuator (VCA) to control precisely the separation velocity of
CubeSats with different masses. This article proposes a novel VCA with a new structure of …
CubeSats with different masses. This article proposes a novel VCA with a new structure of …
Relative reachable domain for spacecraft with initial state uncertainties
The reachable domain is a geometric description of the maneuverability of a spacecraft
under control and/or measurement uncertainties. In this paper, the reachable domain …
under control and/or measurement uncertainties. In this paper, the reachable domain …
Fabrication and testing of the cold gas propulsion system flight unit for the adelis-SAMSON nano-satellites
M Zaberchik, DR Lev, E Edlerman, A Kaidar - Aerospace, 2019 - mdpi.com
Adelis-SAMSON is a nano-satellite mission aimed at performing geo-location of target
signals on Earth using a tight three-satellite formation in space. To maintain formation, each …
signals on Earth using a tight three-satellite formation in space. To maintain formation, each …
Armature Reaction Analysis and Suppression of Voice Coil Actuator Based on an Improved Magnetic Equivalent Circuit Model
Y Zhao, H Yue, J Zhu, F Yang - IEEE Transactions on Industrial …, 2023 - ieeexplore.ieee.org
The high thrust density voice coil actuator (VCA) is a key component for the deployers to
determine the CubeSats' separation velocity in orbit directly. To improve the VCA's thrust …
determine the CubeSats' separation velocity in orbit directly. To improve the VCA's thrust …
Cluster-keeping algorithms for the satellite swarm sensor network project
E Edlerman, P Gurfil - Journal of Spacecraft and Rockets, 2019 - arc.aiaa.org
This paper develops cluster control algorithms for the Satellite Swarm Sensor Network
project, for which the main aim is to enable disaggregation of space-based remote sensing …
project, for which the main aim is to enable disaggregation of space-based remote sensing …
Three-dimensional relative reachable domain with initial state uncertainty in Gaussian distribution
C Wen, Y Gao, H Shi - Proceedings of the Institution of …, 2019 - journals.sagepub.com
A probability threshold is a confidence level defining a bound outside which the occurrence
of a random variable is considered as a rare event. Upon providing such a probability …
of a random variable is considered as a rare event. Upon providing such a probability …
[HTML][HTML] 航天器近距离相对运动的轨迹偏差分析
石昊, 赵育善, 师鹏 - 2017 - html.rhhz.net
利用相对可达区(RRD) 的概念对航天器在脉冲闭环控制方式下相对运动的轨迹偏差进行了分析.
相对可达区是对航天器可能出现位置集合的一种几何描述. 当航天器的状态误差服从高斯分布时 …
相对可达区是对航天器可能出现位置集合的一种几何描述. 当航天器的状态误差服从高斯分布时 …