The attitude control problem, or the control of a spacecraft's orientation with respect to a frame of reference, is a challenging problem in space missions and has attracted much attention as it involves highly nonlinear characteristics of the governing equations. The attitude control task requires an estimation algorithm that deduces the attitude from strapdown sensor inputs and a control algorithm that computes the necessary torques so that the vehicle can follow a desired attitude.From the perspective of control, feedback control laws are sought for the purpose of asymptotic trajectory tracking, with the ability to reject unexpected external disturbances, and be insensitive to parameter variations. An adaptive sliding mode spacecraft att...
In this paper the problem of attitude tracking control for a rigid spacecraft is addressed. It is as...
The main objective of this research is to provide attitude estimation, orbit estimation, and attitud...
The University of Illinois’s IlliniSat2 satellite bus is unique in that it is among only a few nano-...
In this thesis novel feedback attitude control algorithms and attitude estimation algorithms are dev...
Increasing the computational efficiency of attitude estimation is a critical problem related to mode...
In this paper, we present a case study on spacecraft attitude control. The plant (spacecraft attitud...
In order to meet requirements in terms of robustness, stability, and performance for future generati...
International audienceThis brief proposes new algorithms for attitude estimation and control, based ...
Attitude estimation is one of the basic processes of the attitude and orbit control system hosted by...
New advanced control techniques for attitude determination and control of small (micro) satellites a...
Various control design techniques are model dependent. They typically require knowledge of the inert...
AbstractAimed at low accuracy of attitude determination because of using low-cost components which m...
In this paper the problem of attitude tracking control for a rigid spacecraft is addressed. It is as...
A nonlinear control scheme using a Modified State-Dependent Riccati Equation (MSDRE) is developed th...
We consider the attitude and gyro-bias estimation as well as the attitude stabilization problem of a...
In this paper the problem of attitude tracking control for a rigid spacecraft is addressed. It is as...
The main objective of this research is to provide attitude estimation, orbit estimation, and attitud...
The University of Illinois’s IlliniSat2 satellite bus is unique in that it is among only a few nano-...
In this thesis novel feedback attitude control algorithms and attitude estimation algorithms are dev...
Increasing the computational efficiency of attitude estimation is a critical problem related to mode...
In this paper, we present a case study on spacecraft attitude control. The plant (spacecraft attitud...
In order to meet requirements in terms of robustness, stability, and performance for future generati...
International audienceThis brief proposes new algorithms for attitude estimation and control, based ...
Attitude estimation is one of the basic processes of the attitude and orbit control system hosted by...
New advanced control techniques for attitude determination and control of small (micro) satellites a...
Various control design techniques are model dependent. They typically require knowledge of the inert...
AbstractAimed at low accuracy of attitude determination because of using low-cost components which m...
In this paper the problem of attitude tracking control for a rigid spacecraft is addressed. It is as...
A nonlinear control scheme using a Modified State-Dependent Riccati Equation (MSDRE) is developed th...
We consider the attitude and gyro-bias estimation as well as the attitude stabilization problem of a...
In this paper the problem of attitude tracking control for a rigid spacecraft is addressed. It is as...
The main objective of this research is to provide attitude estimation, orbit estimation, and attitud...
The University of Illinois’s IlliniSat2 satellite bus is unique in that it is among only a few nano-...