Pages that link to "Item:Q2348202"

The following pages link to Robust fault-tolerant control for flexible spacecraft against partial actuator failures (Q2348202):

Displaying 31 items.

• Electrodynamic attitude stabilization of a satellite in the Konig frame (Q330806) (← links)
• Dual-quaternion-based adaptive motion tracking of spacecraft with reduced control effort (Q331254) (← links)
• Partial stability analysis of nonlinear nonstationary systems via averaging (Q345859) (← links)
• Reliable sampled-data vibration control for uncertain flexible spacecraft with frequency range limitation (Q345931) (← links)
• Fault-tolerant sliding mode attitude control for flexible spacecraft under loss of actuator effectiveness (Q395166) (← links)
• Fault-tolerant sampled-data control of flexible spacecraft with probabilistic time delays (Q494756) (← links)
• On the attitude stabilization of a rigid spacecraft using two skew control moment gyros (Q494779) (← links)
• Active fault tolerant control design approach for the flexible spacecraft with sensor faults (Q682679) (← links)
• Robust synthesized control of electromechanical actuator for thrust vector system in spacecraft (Q745746) (← links)
• Distributed attitude control for multiple flexible spacecraft under actuator failures and saturation (Q1676853) (← links)
• Anti-disturbance fault-tolerant attitude control for satellites subject to multiple disturbances and actuator saturation (Q1687347) (← links)
• Robust control allocation for spacecraft attitude stabilization under actuator faults and uncertainty (Q1719133) (← links)
• Fuzzy logic based fault-tolerant attitude control for nonlinear flexible spacecraft with sampled-data input (Q1796578) (← links)
• Finite-time reliable attitude tracking control design for nonlinear quadrotor model with actuator faults (Q2050432) (← links)
• Fault-tolerant control for the linearized spacecraft attitude control system with Markovian switching (Q2096114) (← links)
• Composite fault tolerant attitude control for flexible satellite system under disturbance and input delay (Q2244188) (← links)
• Fault tolerant tracking of Mars entry vehicles via fuzzy control approach (Q2328970) (← links)
• Fuzzy predictive fault-tolerant control for time-delay nonlinear systems with partial actuator failures (Q2336024) (← links)
• Robust finite-time non-fragile sampled-data control for T-S fuzzy flexible spacecraft model with stochastic actuator faults (Q2423072) (← links)
• Decentralized asymptotic fault tolerant control of near space vehicle with high order actuator dynamics (Q2451861) (← links)
• Robustness properties of collocated controllers for flexible spacecraft (Q3728771) (← links)
• Optimisation of controller reconfiguration instant for spacecraft control systems with additive actuator faults (Q5029168) (← links)
• (Q5209183) (← links)
• Finite‐time prescribed performance adaptive fuzzy fault‐tolerant control for nonstrict‐feedback nonlinear systems (Q5241015) (← links)
• Continuous robust fault‐tolerant control and vibration suppression for flexible spacecraft without angular velocity (Q5241719) (← links)
• Adaptive fixed‐time fault‐tolerant control for rigid spacecraft using a double power reaching law (Q5241725) (← links)
• Velocity-free fault-tolerant control allocation for flexible spacecraft with redundant thrusters (Q5252889) (← links)
• Decentralized Robust Servomechanism Problem for Large Flexible Space Structures Under Sensor and Actuator Failures (Q5353059) (← links)
• Active fault‐tolerant attitude control for flexible spacecraft with loss of actuator effectiveness (Q5745666) (← links)
• Stochastic fuzzy predictive fault‐tolerant control for time‐delay nonlinear system with actuator fault under a certain probability (Q6078860) (← links)
• Event-based fault-tolerant \(H_\infty\) synchronization for inertial neural networks via a semi-Markov jump approach (Q6082825) (← links)