Research graph
References from Spacecraft attitude control via high-order fully actuated system approach and fuzzy logic system: Theory, simulation, and air-bearing experiments. Local targets link to admitted publications; unresolved targets remain external evidence.
10.1016/j.ast.2023.108134
10.1016/j.ast.2023.108134 · External reference
10.1016/j.ast.2025.110197
10.1016/j.ast.2025.110197 · External reference
10.1016/j.ast.2023.108220
10.1016/j.ast.2023.108220 · External reference
Self-distillation adaptive pose estimation method for cross-domain non-cooperative spacecraft based on optical sensor data
10.1109/jsen.2025.3615727 · 2025 · External reference
Adaptive fuzzy fault-tolerant attitude control of spacecraft
10.1016/j.conengprac.2010.08.005 · 2011 · External reference
10.1016/j.conengprac.2025.106373
10.1016/j.conengprac.2025.106373 · External reference
Sliding mode control techniques and artificial potential field for dynamic collision avoidance in rendezvous maneuvers
10.1109/lcsys.2019.2926053 · 2020 · External reference
Online test-time adaptation for on-orbit non-cooperative spacecraft pose estimation
2025 · External reference
Adaptive fault-tolerant attitude control for satellite reorientation under input saturation
10.1016/j.ast.2018.04.015 · 2018 · External reference
Spacecraft formation and orbit control using differential attitude-dependent solar radiation pressure
10.1016/j.asr.2020.03.047 · 2021 · External reference
Fast fixed-time attitude tracking control of spacecraft with prescribed performance
10.1002/rnc.6638 · 2023 · External reference
Robust adaptive predefined time prescribed performance attitude control for spacecraft
10.1016/j.conengprac.2025.106271 · 2025 · External reference
Interval uncertainty-oriented optimal control method for spacecraft attitude control
2023 · External reference
Adaptive sliding mode and RBF neural network based fault tolerant attitude control for spacecraft with unknown uncertainties and disturbances
10.1016/j.asr.2024.05.021 · 2024 · External reference
A novel predictor based optimal integral sliding-mode-based attitude tracking control of spacecraft under actuator’s uncertainties and constraints
10.1016/j.conengprac.2025.106269 · 2025 · External reference
Attitude control of spacecraft simulator without angular velocity measurement
10.1016/j.conengprac.2018.11.011 · 2019 · External reference
Extended state filter-based velocity-free finite-time attitude control of spacecraft
10.1002/rnc.7264 · 2024 · External reference
Velocity-free adaptive nonsingular fast terminal sliding mode finite-time attitude tracking control for spacecraft
10.1002/asjc.3051 · 2023 · External reference
Dynamic event-triggered gain-scheduled output feedback control for LPV systems with application to morphing aircraft
10.1109/tase.2026.3717504 · 2026 · External reference
10.1016/j.ast.2026.113270
10.1016/j.ast.2026.113270 · External reference
High-order system approaches-I. Fully-actuated systems and parametric designs
2020 · External reference
Output position control of two-mass systems based on fully actuated system and singular perturbation approaches
10.1109/tmech.2025.3602374 · 2026 · External reference
High-order fully actuated approach for output tracking control of flexible servo systems subject to uncertainties and disturbances
10.1109/tie.2025.3531480 · 2025 · External reference
Attitude control of spherical liquid-filled spacecraft based on high-order fully actuated system approaches
10.1007/s11424-022-2055-y · 2022 · External reference
Twistors-based attitude-orbit integrated control for spacecraft: a high-order fully actuated system approach
10.1109/tsmc.2024.3519436 · 2025 · External reference
Fixed-time fault-tolerant attitude consensus control for multiple spacecraft via fully actuated system approaches
10.1007/s11071-025-11598-y · 2025 · External reference
Event-triggered adaptive fuzzy asymptotic tracking control for rigid spacecraft attitude systems with full-state constraints and disturbances
10.1109/taes.2024.3369006 · 2024 · External reference
Adaptive fuzzy resilient decentralized control for nonlinear large-scale CPSS under DoS attacks
2024 · External reference
Dynamic event-triggered gain-scheduled H∞ control for a polytopic LPV model of morphing aircraft
10.1109/taes.2024.3440966 · 2025 · External reference
Predefined-time sliding mode control with neural network observer for hypersonic morphing vehicles
10.1109/taes.2025.3570262 · 2025 · External reference
Adaptive fuzzy control of spacecraft proximity operations using hierarchical fuzzy systems
10.1109/tmech.2015.2494607 · 2016 · External reference
Velocity observer-based event-triggered adaptive fuzzy attitude takeover control of spacecraft with quantized quaternion
10.1109/taes.2023.3237127 · 2023 · External reference
Integrated attitude-orbit control for spacecraft with prescribed performance via fully actuated system approach
10.1109/taes.2025.3637795 · 2026 · External reference
Attitude–orbit integrated modeling and control for flexible spacecraft based on Twistors and fully actuated system approach
10.1109/tsmc.2025.3647684 · 2026 · External reference
Predictive control of discrete-time high-order fully actuated systems with application to air-bearing spacecraft simulator
10.1016/j.jfranklin.2023.04.003 · 2023 · External reference
Velocity-free adaptive nonsingular fast terminal sliding mode finite-time attitude tracking control for spacecraft
10.1002/asjc.3051 · ExternalCitation · doi-reference
Fast fixed-time attitude tracking control of spacecraft with prescribed performance
10.1002/rnc.6638 · ExternalCitation · doi-reference
Extended state filter-based velocity-free finite-time attitude control of spacecraft
10.1002/rnc.7264 · ExternalCitation · doi-reference
Fixed-time fault-tolerant attitude consensus control for multiple spacecraft via fully actuated system approaches
10.1007/s11071-025-11598-y · ExternalCitation · doi-reference
Attitude control of spherical liquid-filled spacecraft based on high-order fully actuated system approaches
10.1007/s11424-022-2055-y · ExternalCitation · doi-reference
Spacecraft formation and orbit control using differential attitude-dependent solar radiation pressure
10.1016/j.asr.2020.03.047 · ExternalCitation · doi-reference
Adaptive sliding mode and RBF neural network based fault tolerant attitude control for spacecraft with unknown uncertainties and disturbances
10.1016/j.asr.2024.05.021 · ExternalCitation · doi-reference
Adaptive fault-tolerant attitude control for satellite reorientation under input saturation
10.1016/j.ast.2018.04.015 · ExternalCitation · doi-reference
10.1016/j.ast.2023.108134
10.1016/j.ast.2023.108134 · ExternalCitation · doi-reference
10.1016/j.ast.2023.108220
10.1016/j.ast.2023.108220 · ExternalCitation · doi-reference
10.1016/j.ast.2025.110197
10.1016/j.ast.2025.110197 · ExternalCitation · doi-reference
10.1016/j.ast.2026.113270
10.1016/j.ast.2026.113270 · ExternalCitation · doi-reference
Adaptive fuzzy fault-tolerant attitude control of spacecraft
10.1016/j.conengprac.2010.08.005 · ExternalCitation · doi-reference
Attitude control of spacecraft simulator without angular velocity measurement
10.1016/j.conengprac.2018.11.011 · ExternalCitation · doi-reference
A novel predictor based optimal integral sliding-mode-based attitude tracking control of spacecraft under actuator’s uncertainties and constraints
10.1016/j.conengprac.2025.106269 · ExternalCitation · doi-reference
Robust adaptive predefined time prescribed performance attitude control for spacecraft
10.1016/j.conengprac.2025.106271 · ExternalCitation · doi-reference
10.1016/j.conengprac.2025.106373
10.1016/j.conengprac.2025.106373 · ExternalCitation · doi-reference
Predictive control of discrete-time high-order fully actuated systems with application to air-bearing spacecraft simulator
10.1016/j.jfranklin.2023.04.003 · ExternalCitation · doi-reference
Self-distillation adaptive pose estimation method for cross-domain non-cooperative spacecraft based on optical sensor data
10.1109/jsen.2025.3615727 · ExternalCitation · doi-reference
Sliding mode control techniques and artificial potential field for dynamic collision avoidance in rendezvous maneuvers
10.1109/lcsys.2019.2926053 · ExternalCitation · doi-reference
Velocity observer-based event-triggered adaptive fuzzy attitude takeover control of spacecraft with quantized quaternion
10.1109/taes.2023.3237127 · ExternalCitation · doi-reference
Event-triggered adaptive fuzzy asymptotic tracking control for rigid spacecraft attitude systems with full-state constraints and disturbances
10.1109/taes.2024.3369006 · ExternalCitation · doi-reference
Dynamic event-triggered gain-scheduled H∞ control for a polytopic LPV model of morphing aircraft
10.1109/taes.2024.3440966 · ExternalCitation · doi-reference
Predefined-time sliding mode control with neural network observer for hypersonic morphing vehicles
10.1109/taes.2025.3570262 · ExternalCitation · doi-reference
Integrated attitude-orbit control for spacecraft with prescribed performance via fully actuated system approach
10.1109/taes.2025.3637795 · ExternalCitation · doi-reference
Dynamic event-triggered gain-scheduled output feedback control for LPV systems with application to morphing aircraft
10.1109/tase.2026.3717504 · ExternalCitation · doi-reference
High-order fully actuated approach for output tracking control of flexible servo systems subject to uncertainties and disturbances
10.1109/tie.2025.3531480 · ExternalCitation · doi-reference
Adaptive fuzzy control of spacecraft proximity operations using hierarchical fuzzy systems
10.1109/tmech.2015.2494607 · ExternalCitation · doi-reference
Output position control of two-mass systems based on fully actuated system and singular perturbation approaches
10.1109/tmech.2025.3602374 · ExternalCitation · doi-reference
Twistors-based attitude-orbit integrated control for spacecraft: a high-order fully actuated system approach
10.1109/tsmc.2024.3519436 · ExternalCitation · doi-reference
Attitude–orbit integrated modeling and control for flexible spacecraft based on Twistors and fully actuated system approach
10.1109/tsmc.2025.3647684 · ExternalCitation · doi-reference
