176 p.In this thesis, we study the robust optimal attitude control problem of microsatellites with disturbances and an uncertain inertia matrix. This is a nonlinear control problem. As the emphasis is on the development of state-feedback attitude controllers that achieve optimality as well as disturbance attenuation, a brief survey is made of the Lyapunov stability and the disturbance attenuation problems of nonlinear systems.DOCTOR OF PHILOSOPHY (EEE
Controllers are often designed based on the assumption that a control actuation can be directly appl...
Since the development of the CubeSat standard, the number of nanosatellites developed by universitie...
The paper deals with the problem of the magnetic attitude control for microsatellite in LEO, with th...
This report summarizes the research work carried out in the AcRF project RG 9/00 Attitude Control o...
Attitude control and stabilization of a micro-satellite is a nontrivial problem due to the highly no...
In this paper, the non-fragile robust attitude control problem is investigated for flexible microsat...
In this paper, we deal with the attitude control of a satellite equipped with wheels of reaction, us...
This paper proposes a robust optimal attitude control design for multiple-input, multiple-output (MI...
This paper deals with the attitude dynamics and control of a multimission microsatellite for remote ...
In this paper, we present a case study on spacecraft attitude control. The plant (spacecraft attitud...
SMART (Scientific Microsatellite for Advanced Research and Technology) is a project of the two Unive...
While nonlinear attitude control has been explored widely in theory, nanosatellite air-bearing-based...
In the context of the initiative Formation for Atmospheric Science and Technology demonstration (FAS...
In order to meet requirements in terms of robustness, stability, and performance for future generati...
Actuator failures onboard spacecraft often lead to unsatisfied control performances or even the lose...
Controllers are often designed based on the assumption that a control actuation can be directly appl...
Since the development of the CubeSat standard, the number of nanosatellites developed by universitie...
The paper deals with the problem of the magnetic attitude control for microsatellite in LEO, with th...
This report summarizes the research work carried out in the AcRF project RG 9/00 Attitude Control o...
Attitude control and stabilization of a micro-satellite is a nontrivial problem due to the highly no...
In this paper, the non-fragile robust attitude control problem is investigated for flexible microsat...
In this paper, we deal with the attitude control of a satellite equipped with wheels of reaction, us...
This paper proposes a robust optimal attitude control design for multiple-input, multiple-output (MI...
This paper deals with the attitude dynamics and control of a multimission microsatellite for remote ...
In this paper, we present a case study on spacecraft attitude control. The plant (spacecraft attitud...
SMART (Scientific Microsatellite for Advanced Research and Technology) is a project of the two Unive...
While nonlinear attitude control has been explored widely in theory, nanosatellite air-bearing-based...
In the context of the initiative Formation for Atmospheric Science and Technology demonstration (FAS...
In order to meet requirements in terms of robustness, stability, and performance for future generati...
Actuator failures onboard spacecraft often lead to unsatisfied control performances or even the lose...
Controllers are often designed based on the assumption that a control actuation can be directly appl...
Since the development of the CubeSat standard, the number of nanosatellites developed by universitie...
The paper deals with the problem of the magnetic attitude control for microsatellite in LEO, with th...
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