A nonlinear adaptive control law for the attitude control of satellites using gyrotorquers is presented. The derivation of the control law does not require any information on the system dynamics and the environmental disturbance torques acting on the satellite. A simplified control law for spinning satellites is derived. The controller requires only attitude tracking error and its derivative for feedback. Simulation results are presented which show that, in the closed-loop system, precise attitude control can be accomplished in spite of the uncertainty in the syste
Spacecraft and interplanetary probes orbiting at high altitudes experience forces due to solar radia...
Thousands of satellites are now in operation for various purposes such as communication, navigation,...
M. Tech. Electrical EngineeringDeals with nonlinear methods for magnetic attitude control and reacti...
A nonlinear adaptive control law for the attitude control of satellites using gyrotorquers is presen...
A model reference adaptive control law is presented for large angle rotational maneuvers of spacecra...
In this paper two nonlinear control techniques are developed and compared for the satellite attitude...
In this paper two nonlinear control techniques are developed and compared for the satellite attitude...
A control law is presented for asymptotic function reproducibility in a class of nonlinear-systems s...
Spacecraft and interplanetary probes orbiting at high altitudes experience forces due to solar radia...
A nonlinear adaptive attitude controller is designed in this paper that compensates for dynamic unce...
A nonlinear adaptive attitude controller is designed in this paper that compensates for dynamic unce...
A nonlinear control law for large angle rotational maneuvers of spacecraft using reaction wheels in ...
In this paper, a nonlinear direct adaptive output control methodology is developed to address the pr...
Recently developed results for direct adaptive control design in the context of uncertain systems in...
This paper considers the problem of reaction-wheel attitude control inside the mission mode of the M...
Spacecraft and interplanetary probes orbiting at high altitudes experience forces due to solar radia...
Thousands of satellites are now in operation for various purposes such as communication, navigation,...
M. Tech. Electrical EngineeringDeals with nonlinear methods for magnetic attitude control and reacti...
A nonlinear adaptive control law for the attitude control of satellites using gyrotorquers is presen...
A model reference adaptive control law is presented for large angle rotational maneuvers of spacecra...
In this paper two nonlinear control techniques are developed and compared for the satellite attitude...
In this paper two nonlinear control techniques are developed and compared for the satellite attitude...
A control law is presented for asymptotic function reproducibility in a class of nonlinear-systems s...
Spacecraft and interplanetary probes orbiting at high altitudes experience forces due to solar radia...
A nonlinear adaptive attitude controller is designed in this paper that compensates for dynamic unce...
A nonlinear adaptive attitude controller is designed in this paper that compensates for dynamic unce...
A nonlinear control law for large angle rotational maneuvers of spacecraft using reaction wheels in ...
In this paper, a nonlinear direct adaptive output control methodology is developed to address the pr...
Recently developed results for direct adaptive control design in the context of uncertain systems in...
This paper considers the problem of reaction-wheel attitude control inside the mission mode of the M...
Spacecraft and interplanetary probes orbiting at high altitudes experience forces due to solar radia...
Thousands of satellites are now in operation for various purposes such as communication, navigation,...
M. Tech. Electrical EngineeringDeals with nonlinear methods for magnetic attitude control and reacti...