Pages that link to "Item:Q2249678"

The following pages link to Controller design for rigid spacecraft attitude tracking with actuator saturation (Q2249678):

Displaying 50 items.

• Robust \(H_\infty\) control for uncertain singular discrete T-S fuzzy time-delay systems with actuator saturation (Q308312) (← links)
• Robust control for Markovian jump delta operator systems with actuator saturation (Q397597) (← links)
• Actuator failure compensation and attitude control for rigid satellite by adaptive control using quaternion feedback (Q398367) (← links)
• Design of the microsatellite attitude control system using the mixed method via LMI optimization (Q460362) (← links)
• A second-order sliding mode controller design for spacecraft tracking control (Q473654) (← links)
• Using of H-infinity control method in attitude control system of rigid-flexible satellite (Q613793) (← links)
• Robust fuzzy-scheduling control for nonlinear systems subject to actuator saturation via delta operator approach (Q726354) (← links)
• A robust attitude control strategy with guaranteed transient performance via modified Lyapunov-based control and integral sliding mode control (Q748099) (← links)
• Finite-time attitude control for rigid spacecraft subject to actuator saturation (Q783550) (← links)
• Active disturbance rejection control for high pointing accuracy and rotation speed (Q963779) (← links)
• Adaptive robust tracking for flexible spacecraft in presence of disturbances (Q1273906) (← links)
• Adaptive terminal sliding mode based thruster fault tolerant control for underwater vehicle in time-varying ocean currents (Q1660724) (← links)
• A mixed variable speed reaching law of sliding mode control for spacecraft tracking system (Q1665483) (← links)
• Stochastic finite-time boundedness on switching dynamics Markovian jump linear systems with saturated and stochastic nonlinearities (Q1671287) (← links)
• Comments on ``Controller design for rigid spacecraft attitude tracking with actuator saturation'' (Q1671723) (← links)
• Anti-disturbance fault-tolerant attitude control for satellites subject to multiple disturbances and actuator saturation (Q1687347) (← links)
• \(H_{\infty}\) static output tracking control of nonlinear systems with one-sided Lipschitz condition (Q1719057) (← links)
• Adaptive finite-time command filtered fault-tolerant control for uncertain spacecraft with prescribed performance (Q1723035) (← links)
• Output feedback control for asymptotic stabilization of spacecraft with input saturation (Q1794217) (← links)
• Practical stabilization of delta operator systems subject to actuator saturation and disturbances (Q1796585) (← links)
• Sliding mode attitude tracking of rigid spacecraft with disturbances (Q1933433) (← links)
• Design of attitude control systems for cubesat-class nanosatellite (Q1953735) (← links)
• Attitude-tracking control with path planning for agile satellite using double-gimbal control moment gyros (Q1954672) (← links)
• Parametric delta operator Riccati equation and applications to semi-global stabilization in the presence of actuator saturation (Q2011857) (← links)
• Passivity-based adaptive tracking control of spacecraft line-of-sight relative motion with thrust saturation (Q2047077) (← links)
• Fully actuated system approach for 6DOF spacecraft control based on extended state observer (Q2165411) (← links)
• Fully-actuated system approach based optimal attitude tracking control of rigid spacecraft with actuator saturation (Q2165418) (← links)
• Nonsingular fast terminal adaptive neuro-sliding mode control for spacecraft formation flying systems (Q2187065) (← links)
• An anti-windup method for a class of uncertain MIMO systems subject to actuator saturation with LADRC (Q2198253) (← links)
• Fixed-time control for high-precision attitude stabilization of flexible spacecraft (Q2220082) (← links)
• Robust chattering-free finite time attitude tracking control with input saturation (Q2287373) (← links)
• Attitude control of rigid spacecraft with disturbance generated by time varying exosystems (Q2299872) (← links)
• Spacecraft output feedback attitude control based on extended state observer and adaptive dynamic programming (Q2423888) (← links)
• System identification and multivariable control design for a satellite ultraquiet isolation technology experiment (SUITE) (Q2511892) (← links)
• Decentralised finite-time attitude synchronisation and tracking control for rigid spacecraft (Q2792186) (← links)
• A simple saturated control framework for spacecraft with bounded disturbances (Q2792781) (← links)
• Robust attitude tracking control of spacecraft under control input magnitude and rate saturations (Q2798390) (← links)
• Stability analysis for delta operator systems subject to state saturation (Q2821388) (← links)
• Analysis and design of delta operator systems with nested actuator saturation (Q2821389) (← links)
• Stabilization on null controllable region of delta operator systems subject to actuator saturation (Q2835515) (← links)
• Quantized stabilization of networked control systems with actuator saturation (Q2835522) (← links)
• Null controllable region of delta operator systems subject to actuator saturation (Q2954035) (← links)
• A Hybrid Scheme of Synthesized Sliding Mode/Strain Rate Feedback Control Design for Flexible Spacecraft Attitude Maneuver Using Time Scale Decomposition (Q2972475) (← links)
• Quaternion-based attitude synchronisation for multiple rigid bodies in the presence of actuator saturation (Q2974200) (← links)
• Nussbaum‐type function–based attitude control of spacecraft with actuator saturation (Q4565997) (← links)
• Spacecraft Anti‐Unwinding Attitude Control Using Second‐Order Sliding Mode (Q4575103) (← links)
• Neural adaptive integral sliding mode control for attitude tracking of flexible spacecraft with signal quantisation and actuator nonlinearity (Q5026585) (← links)
• Extended state observer-based attitude fault-tolerant control of rigid spacecraft (Q5027775) (← links)
• Event-triggered integral sliding mode controller for rigid spacecraft attitude tracking with angular velocity constraint (Q5056567) (← links)
• Dynamic infinity‐norm constrained control allocation for attitude tracking control of overactuated combined spacecraft (Q5221138) (← links)