Add to ORKGIn this thesis, analysis and comparison of different attitude control systems of a satelliteusing different reaction wheel configurations were investigated. Three different reactionwheel configurations (e.g. tetrahedron configuration, pyramid configuration, standardorthogonal 3-wheel configuration) and three control algorithms (Linear Quadratic Regulator,Sliding Mode, Integrator Backstepping) were analyzed and compared in terms of settlingtimes, power consumptions and actuator failure robustness.Validerat; 20121205 (global_studentproject_submitter
Satellite Attitude Determination and Control System (ADCS) uses an active actuator with a Reaction w...
In this research, nonlinear attitude controllers are designed for a low earth orbit satellite intend...
The purpose of this paper is the design and the performance analysis of a control technique that all...
In this thesis, analysis and comparison of different attitude control systems of a satelliteusing di...
The satellite reaction wheel’s configuration plays also an important role in providing the attitude ...
Nowadays, most of the designed satellites are dedicated for high performance missions, which require...
Abstract. Within the motto smaller, cheaper and better, several nations can have now easy access to ...
Attitude determination and control of satellite is important component which determines the accompli...
The purpose of this paper is to identify the low-power Reaction Wheel (RW) configuration for a 3-axi...
This thesis presents a method for fault diagnosis in spacecraft attitude control system. The focus o...
In this paper, a robust attitude control algorithm is developed based on sliding mode control for a ...
This work addresses the attitude control of a satellite by applying MIMO quantitative feedback appro...
Actuator failures onboard satellites have caused severe and even disastrous consequences on several ...
In the last decades, access to space has become more affordable thanks to the introduction of CubeSa...
A nonlinear attitude model of a satellite with thrusters, gravity torquers and a reaction wheel clus...
Satellite Attitude Determination and Control System (ADCS) uses an active actuator with a Reaction w...
In this research, nonlinear attitude controllers are designed for a low earth orbit satellite intend...
The purpose of this paper is the design and the performance analysis of a control technique that all...
In this thesis, analysis and comparison of different attitude control systems of a satelliteusing di...
The satellite reaction wheel’s configuration plays also an important role in providing the attitude ...
Nowadays, most of the designed satellites are dedicated for high performance missions, which require...
Abstract. Within the motto smaller, cheaper and better, several nations can have now easy access to ...
Attitude determination and control of satellite is important component which determines the accompli...
The purpose of this paper is to identify the low-power Reaction Wheel (RW) configuration for a 3-axi...
This thesis presents a method for fault diagnosis in spacecraft attitude control system. The focus o...
In this paper, a robust attitude control algorithm is developed based on sliding mode control for a ...
This work addresses the attitude control of a satellite by applying MIMO quantitative feedback appro...
Actuator failures onboard satellites have caused severe and even disastrous consequences on several ...
In the last decades, access to space has become more affordable thanks to the introduction of CubeSa...
A nonlinear attitude model of a satellite with thrusters, gravity torquers and a reaction wheel clus...
Satellite Attitude Determination and Control System (ADCS) uses an active actuator with a Reaction w...
In this research, nonlinear attitude controllers are designed for a low earth orbit satellite intend...
The purpose of this paper is the design and the performance analysis of a control technique that all...