Fault-tolerant sliding mode attitude control for flexible spacecraft under loss of actuator effectiveness
Authors:
- 9 October 2010
- journal article
- Published by Springer Nature in Nonlinear Dynamics
- Vol. 64 (1-2) , 13-23
Abstract
No abstract availableKeywords
This publication has 21 references indexed in Scilit:
- Quaternion Observer-Based Model-Independent Attitude Tracking Control of SpacecraftJournal of Guidance, Control, and Dynamics, 2009
- New Results for Time-Optimal Three-Axis Reorientation of a Rigid SpacecraftJournal of Guidance, Control, and Dynamics, 2009
- Inertia-Free Spacecraft Attitude Tracking with Disturbance Rejection and Almost Global StabilizationJournal of Guidance, Control, and Dynamics, 2009
- Nonlinear H_infinity Control Designs with Axisymmetric Spacecraft ControlJournal of Guidance, Control, and Dynamics, 2009
- Adaptive attitude control of spacecraft using neural networksActa Astronautica, 2009
- High-Performance Spacecraft Adaptive Attitude-Tracking Control Through Attracting-Manifold DesignJournal of Guidance, Control, and Dynamics, 2008
- Robust adaptive sliding mode attitude maneuvering and vibration damping of three-axis-stabilized flexible spacecraft with actuator saturation limitsNonlinear Dynamics, 2008
- Optimal Variable-Structure Control Tracking of Spacecraft ManeuversJournal of Guidance, Control, and Dynamics, 2000
- Angular Velocity Stabilization of a Rigid Body Via VSS ControlJournal of Dynamic Systems, Measurement, and Control, 2000
- Smooth sliding-mode control for spacecraft attitude tracking maneuversJournal of Guidance, Control, and Dynamics, 1995