Uncertain optimal attitude control for space power satellite based on interval Riccati equation with non-probabilistic time-dependent reliability

C Yang, W Lu, Y Xia - Aerospace Science and Technology, 2023 - Elsevier
Considering the multi-source uncertainties and disturbances in the attitude dynamics of
space power satellite (SPS), an interval dynamic model of SPS is proposed based on the …

A review of dynamic analysis on space solar power station

W Hu, Z Deng - Astrodynamics, 2023 - Springer
The concept of a space solar power station (SSPS) was proposed in 1968 as a potential
approach for solving the energy crisis. In the past 50 years, several structural concepts have …

Convex set reliability-based optimal attitude control for space solar power station with bounded and correlated uncertainties

C Yang, J Wu, Z Fan, W Lu - Chaos, Solitons & Fractals, 2025 - Elsevier
Considering the bounded and correlated uncertainties in the inherently nonlinear attitude
dynamics, this paper proposes an uncertain optimal attitude control for space solar power …

Multibody dynamics and robust attitude control of a MW-level solar power satellite

K Zhang, S Wu, Z Wu - Aerospace Science and Technology, 2021 - Elsevier
This paper addresses the multibody dynamics and robust attitude control of a MW-level solar
power satellite, which mainly consists of an 800-m-length center truss, a 150-m-diam …

Decentralized fault-tolerant control for satellite attitude synchronization

J Li, KD Kumar - IEEE Transactions on Fuzzy Systems, 2011 - ieeexplore.ieee.org
This paper presents a decentralized adaptive fuzzy approximation design to achieve attitude
tracking control for formation flying in the presence of external disturbances and actuator …

Distributed attitude tracking for multiple flexible spacecraft described by partial differential equations

T Chen, H Wen, Z Wei - Acta astronautica, 2019 - Elsevier
In this study, two distributed control strategies without or with a Partial Differential Equation
(PDE) observer are proposed for a team of flexible spacecraft to track the attitude of a virtual …

Conceptual design and orbit-attitude coupled analyses of free-drift solar power satellite

X Chen, R Yuan, J Zhu, C Liu, J Li, Q Li - Advances in Space Research, 2023 - Elsevier
Solar power satellite is known as a promising source of clean energy from space in the
future. One of the key problems of current solar power satellite concepts is the huge cost …

Nonlinear dynamic modeling for analysis of large spacecraft with extendible appendages

T Sun, S Zhang, L Du, L Niu, Q Li, Z Deng - Applied Mathematical Modelling, 2023 - Elsevier
A nonlinear dynamic model of a large spacecraft with extendible ultra-flexible appendages
under the perturbation of gravity gradient that can capture large deformation is proposed in …

空间刚性杆--弹簧组合结构轨道, 姿态耦合动力学分析

尹婷婷, 邓子辰, 胡伟鹏, 李庆军, 曹珊珊 - 力学学报, 2018 - lxxb.cstam.org.cn
以空间太阳帆塔在轨运行中遇到的强耦合动力学问题为研究背景, 建立了空间刚性杆--
弹簧组合结构轨道与姿态耦合问题的动力学模型, 采用辛(几何) 算法研究了其轨道与姿态耦合的 …

Unified modeling method for large space structures using absolute nodal coordinate

Q Li, Z Deng, K Zhang, H Huang - AIAA Journal, 2018 - arc.aiaa.org
A unified rigid-flexible coupled modeling method for large flexible space structures is
proposed based on absolute nodal coordinate formulation (ANCF). The explicit formulas of …