We develop tracking control laws for a rigid spacecraft using both thrusters and momentum wheels. The model studied comprises a rigid body with external thrusters and with N rigid axisymmetric wheels controlled by axial torques. The thruster torques and the axial motor torques are the controls used to track given attitude motions. Specifically, the thruster torques are used to implement the coarse tracking, and the momentum wheels are used to provide the fine control
This thesis addresses sub-optimal employment of 3 momentum wheels for large angle reorientation of r...
The aim of this paper is the analysis of simultaneous attitude control and momentum-wheel management...
The aim of this paper is the analysis of simultaneous attitude control and momentum-wheel management...
Tracking control laws are developed for a rigid spacecraft using both thrusters and momentum wheels....
This paper explores attitude control algorithms using thrusters and momentum wheels for satellite tr...
This paper addresses the guidance and tracking problem for a rigid-spacecraft using two reaction whe...
A control law for an integrated power/attitude control system (IPACS) for a satellite is presented. ...
This paper explores attitude control algorithms using thrusters and momentum wheels for satellite tr...
Recovery control methods have been proposed to tolerate the failure of the thrusters used in the att...
This thesis investigates the control of motion for a general class of vehicles that rotate and trans...
It is well known that three momentum wheel actuators can be used to control the attitude of a rigid ...
In this thesis, we study the problem of designing a practical stabilizer for a rigid body equipped w...
This paper addresses the noncooperative attitude tracking control problem for rigid bodies whose dyn...
This paper investigates the performance of three types of fixed-gain and adap-tive control laws that...
This paper presents innovative mechanisms capable of advantageously providing attitude control for s...
This thesis addresses sub-optimal employment of 3 momentum wheels for large angle reorientation of r...
The aim of this paper is the analysis of simultaneous attitude control and momentum-wheel management...
The aim of this paper is the analysis of simultaneous attitude control and momentum-wheel management...
Tracking control laws are developed for a rigid spacecraft using both thrusters and momentum wheels....
This paper explores attitude control algorithms using thrusters and momentum wheels for satellite tr...
This paper addresses the guidance and tracking problem for a rigid-spacecraft using two reaction whe...
A control law for an integrated power/attitude control system (IPACS) for a satellite is presented. ...
This paper explores attitude control algorithms using thrusters and momentum wheels for satellite tr...
Recovery control methods have been proposed to tolerate the failure of the thrusters used in the att...
This thesis investigates the control of motion for a general class of vehicles that rotate and trans...
It is well known that three momentum wheel actuators can be used to control the attitude of a rigid ...
In this thesis, we study the problem of designing a practical stabilizer for a rigid body equipped w...
This paper addresses the noncooperative attitude tracking control problem for rigid bodies whose dyn...
This paper investigates the performance of three types of fixed-gain and adap-tive control laws that...
This paper presents innovative mechanisms capable of advantageously providing attitude control for s...
This thesis addresses sub-optimal employment of 3 momentum wheels for large angle reorientation of r...
The aim of this paper is the analysis of simultaneous attitude control and momentum-wheel management...
The aim of this paper is the analysis of simultaneous attitude control and momentum-wheel management...