Fault-Tolerant Attitude Control for Flexible Spacecraft With Input Saturation

International Robotics & Automation Journal
doi 10.15406/iratj.2017.02.00026
Full Text
Abstract

Available in full text

Date
Authors
Publisher

MedCrave Group, LLC

Related search

Adaptive Fault-Tolerant Control of Spacecraft Attitude Dynamics With Actuator Failures

Journal of Guidance, Control, and Dynamics
ControlSystems EngineeringElectronic EngineeringApplied MathematicsSpaceElectricalPlanetary ScienceAerospace Engineering
2015English

Sliding Mode Attitude Control for Flexible Spacecraft

2014English

Attitude Maneuvering and Vibration Reducing Control of Flexible Spacecraft Subject to Actuator Saturation and Misalignment

Shock and Vibration
Mechanics of MaterialsGeotechnical EngineeringCondensed Matter PhysicsMechanical EngineeringCivilEngineering GeologyStructural Engineering
2018English

Adaptive Backstepping Attitude Control Law With L2-Gain Performance for Flexible Spacecraft

International Journal of Aerospace Engineering
Aerospace Engineering
2019English

Fuzzy Attitude Control of Flexible Multi-Body Spacecraft

2011English

Adaptive Finite-Time Attitude Control for Spacecraft With Input Quantization and Measurement Uncertainties

Advances in Mechanical Engineering
Mechanical Engineering
2019English

Fault Tolerant Vibration-Attenuation Controller Design for Uncertain Linear Structural Systems With Input Time-Delay and Saturation

Shock and Vibration
Mechanics of MaterialsGeotechnical EngineeringCondensed Matter PhysicsMechanical EngineeringCivilEngineering GeologyStructural Engineering
2013English

Real Time Fault Tolerant Nonlinear Attitude Control System for Nanosatellite Applications

2012English

Fault Tolerant Control of Wind Turbines Using Unknown Input Observers

IFAC Proceedings Volumes
2012English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2024 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy