A survey on formation control of small satellites
GP Liu, S Zhang - Proceedings of the IEEE, 2018 - ieeexplore.ieee.org
This paper comprehensively reviews the state-of-the-art development in formation control of
small satellites. Satellite formation flying, distributed satellite systems, and fractionated …
small satellites. Satellite formation flying, distributed satellite systems, and fractionated …
Finite-time fault-tolerant attitude stabilization for spacecraft with actuator saturation
This paper addresses the finite-time fault-tolerant attitude stabilization control problem for a
rigid spacecraft in the presence of actuator faults or failures, external disturbances, and …
rigid spacecraft in the presence of actuator faults or failures, external disturbances, and …
Fixed-time formation control for spacecraft with prescribed performance guarantee under input saturation
M Zhuang, L Tan, K Li, S Song - Aerospace Science and Technology, 2021 - Elsevier
This paper investigates the fixed-time stability of spacecraft formation flying by considering
input saturation and prescribed performance constraints, including the safe distance …
input saturation and prescribed performance constraints, including the safe distance …
Adaptive fixed-time six-DOF tracking control for noncooperative spacecraft fly-around mission
Y Huang, Y Jia - IEEE Transactions on Control Systems …, 2018 - ieeexplore.ieee.org
This brief is devoted to the fixed-time six-DOF tracking control problem for noncooperative
spacecraft fly-around mission in the presence of the parameters uncertainties and …
spacecraft fly-around mission in the presence of the parameters uncertainties and …
Robust adaptive sliding mode attitude control for aircraft systems based on back-stepping method
In this paper, the robust adaptive control and back-stepping method are considered for
attitude control of aircraft systems. First, a non-linear aircraft model is introduced and …
attitude control of aircraft systems. First, a non-linear aircraft model is introduced and …
New results on sliding-mode control for Takagi–Sugeno fuzzy multiagent systems
This paper investigates the sliding-mode control (SMC) problem of Takagi-Sugeno (TS)
fuzzy multiagent systems (MASs). A cooperative fuzzy-based dynamical sliding-mode (SM) …
fuzzy multiagent systems (MASs). A cooperative fuzzy-based dynamical sliding-mode (SM) …
Decentralized finite-time adaptive fault-tolerant synchronization tracking control for multiple UAVs with prescribed performance
This paper is concerned with the decentralized finite-time fault-tolerant attitude
synchronization tracking control problem for multiple unmanned aerial vehicles (multi-UAVs) …
synchronization tracking control problem for multiple unmanned aerial vehicles (multi-UAVs) …
Fault-tolerant adaptive finite-time attitude synchronization and tracking control for multi-spacecraft formation
This paper addresses the attitude synchronization and tracking control (ASTC) for multi-
spacecraft formation system (MFS) under undirected and directed graph. First, a new …
spacecraft formation system (MFS) under undirected and directed graph. First, a new …
[HTML][HTML] Adaptive control for attitude coordination of leader-following rigid spacecraft systems with inertia parameter uncertainties
YUE Xiaokui, XUE Xianghong, WEN Haowei… - Chinese Journal of …, 2019 - Elsevier
This paper studies the leader-following attitude coordination problems of multiple spacecraft
in the presence of inertia parameter uncertainties. To achieve attitude coordination in the …
in the presence of inertia parameter uncertainties. To achieve attitude coordination in the …
Finite-time attitude tracking control for a rigid spacecraft using time-varying terminal sliding mode techniques
L Zhao, Y Jia - International Journal of Control, 2015 - Taylor & Francis
This paper investigates the finite-time attitude tracking control for a rigid spacecraft in the
presence of inertia uncertainties and external disturbances. Two novel time-varying terminal …
presence of inertia uncertainties and external disturbances. Two novel time-varying terminal …