Add to ORKGIn this thesis nonlinear control method techniques are investigated to control the attitude of Low Earth Orbit satellites. Nonlinear control methods are compared with linear control methods. Simulations are done using Matlab and Simulink software and BILSAT-1 parameters are used in the simulations. Reaction wheels are used as the actuator.M.S. - Master of Scienc
The purpose of this paper is the design and the performance analysis of a control technique that all...
In the thesis the analysis and comparison of different Degrees of freedom effecting a CubeSat using ...
The increasing interest of private companies in the aerospace sector has produced a growth of space ...
In this thesis, application of linear control methods to control the attitude of a Low-Earth Orbit s...
M. Tech. Electrical EngineeringDeals with nonlinear methods for magnetic attitude control and reacti...
In this research, nonlinear attitude controllers are designed for a low earth orbit satellite intend...
The paper presents some aspects for synthesis of small satellites attitude control. Thesatellite non...
A nonlinear attitude model of a satellite with thrusters, gravity torquers and a reaction wheel clus...
In this paper two nonlinear control techniques are developed and compared for the satellite attitude...
In this work, attitude control problem of satellites which are assumed to be as rigidbodies is addre...
One of the most important problem in satellite design is that of attitude stabilization and control...
The cost and error of theSatellite Attitude Control System design can be minimize by using ground te...
In this paper two nonlinear control techniques are developed and compared for the satellite attitude...
In this thesis, analysis and comparison of different attitude control systems of a satelliteusing di...
This work addresses the attitude control of a satellite by applying MIMO quantitative feedback appro...
The purpose of this paper is the design and the performance analysis of a control technique that all...
In the thesis the analysis and comparison of different Degrees of freedom effecting a CubeSat using ...
The increasing interest of private companies in the aerospace sector has produced a growth of space ...
In this thesis, application of linear control methods to control the attitude of a Low-Earth Orbit s...
M. Tech. Electrical EngineeringDeals with nonlinear methods for magnetic attitude control and reacti...
In this research, nonlinear attitude controllers are designed for a low earth orbit satellite intend...
The paper presents some aspects for synthesis of small satellites attitude control. Thesatellite non...
A nonlinear attitude model of a satellite with thrusters, gravity torquers and a reaction wheel clus...
In this paper two nonlinear control techniques are developed and compared for the satellite attitude...
In this work, attitude control problem of satellites which are assumed to be as rigidbodies is addre...
One of the most important problem in satellite design is that of attitude stabilization and control...
The cost and error of theSatellite Attitude Control System design can be minimize by using ground te...
In this paper two nonlinear control techniques are developed and compared for the satellite attitude...
In this thesis, analysis and comparison of different attitude control systems of a satelliteusing di...
This work addresses the attitude control of a satellite by applying MIMO quantitative feedback appro...
The purpose of this paper is the design and the performance analysis of a control technique that all...
In the thesis the analysis and comparison of different Degrees of freedom effecting a CubeSat using ...
The increasing interest of private companies in the aerospace sector has produced a growth of space ...