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Dong Ye
Dong Ye
Подтвержден адрес электронной почты в домене hit.edu.cn - Главная страница
Название
Процитировано
Процитировано
Год
Predefined-time predefined-bounded attitude tracking control for rigid spacecraft
D Ye, AM Zou, Z Sun
IEEE Transactions on Aerospace and Electronic Systems 58 (1), 464-472, 2021
1142021
Finite-time relative orbit-attitude tracking control for multi-spacecraft with collision avoidance and changing network topologies
J Zhang, D Ye, JD Biggs, Z Sun
Advances in Space Research 63 (3), 1161-1175, 2019
592019
Extended state observer based robust adaptive control on SE (3) for coupled spacecraft tracking maneuver with actuator saturation and misalignment
J Zhang, D Ye, Z Sun, C Liu
Acta Astronautica 143, 221-233, 2018
592018
Satellite proximate pursuit-evasion game with different thrust configurations
D Ye, M Shi, Z Sun
Aerospace science and technology 99, 105715, 2020
532020
Finite-time attitude set-point tracking for thrust-vectoring spacecraft rendezvous
J Zhang, JD Biggs, D Ye, Z Sun
Aerospace Science and Technology 96, 105588, 2020
532020
Robust filtering for a class of networked nonlinear systems with switching communication channels
L Zhang, X Yin, Z Ning, D Ye
IEEE Transactions on Cybernetics 47 (3), 671-682, 2016
522016
Extended-state-observer-based event-triggered orbit-attitude tracking for low-thrust spacecraft
J Zhang, JD Biggs, D Ye, Z Sun
IEEE Transactions on Aerospace and Electronic Systems 56 (4), 2872-2883, 2019
462019
Robust high-precision attitude control for flexible spacecraft with improved mixed H2/H∞ control strategy under poles assignment constraint
C Liu, D Ye, K Shi, Z Sun
Acta Astronautica 136, 166-175, 2017
452017
Satellite proximate interception vector guidance based on differential games
YE Dong, SHI Mingming, SUN Zhaowei
Chinese Journal of Aeronautics 31 (6), 1352-1361, 2018
402018
Extended state observer–based finite-time controller design for coupled spacecraft formation with actuator saturation
D Ye, J Zhang, Z Sun
Advances in Mechanical Engineering 9 (4), 1687814017696413, 2017
352017
Robust finite time control algorithm for satellite attitude control
Y Li, D Ye, Z Sun
Aerospace science and technology 68, 46-57, 2017
332017
Adaptive fault-tolerant attitude tracking control for flexible spacecraft with guaranteed performance bounds
Y Xiao, A de Ruiter, D Ye, Z Sun
IEEE Transactions on Aerospace and Electronic Systems 58 (3), 1922-1940, 2021
322021
Time efficient sliding mode controller based on Bang–Bang logic for satellite attitude control
Y Li, D Ye, Z Sun
Aerospace science and technology 75, 342-352, 2018
312018
Adaptive fuzzy finite-time control for spacecraft formation with communication delays and changing topologies
J Zhang, D Ye, M Liu, Z Sun
Journal of the Franklin Institute 354 (11), 4377-4403, 2017
312017
Pursuit-evasion game switching strategies for spacecraft with incomplete-information
X Tang, D Ye, L Huang, Z Sun, J Sun
Aerospace Science and Technology 119, 107112, 2021
302021
Adaptive control on SE (3) for spacecraft pose tracking with harmonic disturbance and input saturation
H Zhang, D Ye, Y Xiao, Z Sun
IEEE Transactions on Aerospace and Electronic Systems 58 (5), 4578-4594, 2022
262022
Robust adaptive variable structure tracking control for spacecraft chaotic attitude motion
C Liu, Z Sun, D Ye, K Shi
IEEE Access 6, 3851-3857, 2018
252018
Hybrid thrusters and reaction wheels strategy for large angle rapid reorientation with high precision
D Ye, Z Sun, S Wu
Acta Astronautica 77, 149-155, 2012
242012
Third‐order sliding mode fault‐tolerant control for satellites based on iterative learning observer
Z Zhang, D Ye, B Xiao, Z Sun
Asian Journal of Control 21 (1), 43-51, 2019
232019
Near time-optimal controller based on analytical trajectory planning algorithm for satellite attitude maneuver
L You, Y Dong
Aerospace Science and Technology 84, 497-509, 2019
232019
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