A control law is presented for asymptotic function reproducibility in a class of nonlinear-systems such that the output of the system asympotically tends to a given function. The controller consists of a prefilter and a servocompensator. Based on this result, a nonlinear feedback control law for the attitude control of a satellite containing symmetric rotors, in a circular orbit, is derived. In the closed-loop system, given trajectories of pitch, yaw, and roll angles are asymptotically followed, and set point control of attitude is accomplished. Digital simulation results are presented to show the capability of the nonlinear controller
A nonlinear control scheme for attitude control of a spacecraft is combined with a nonlinear gyro bi...
The paper deals with asymptotic tracking of a reference attitude trajectory for rigid spacecraft. Ba...
This article has adopted an analytical method to obtain a non-linear control law to reach the expone...
A control law is presented for asymptotic function reproducibility in a class of nonlinear-systems s...
A nonlinear adaptive control law for the attitude control of satellites using gyrotorquers is presen...
In this paper, we present a case study on spacecraft attitude control. The plant (spacecraft attitud...
In this paper two nonlinear control techniques are developed and compared for the satellite attitude...
A nonlinear control law for large angle rotational maneuvers of spacecraft using reaction wheels in ...
In this paper we consider the problem of controlling the orientation of a satellite with thrusters w...
In this paper two nonlinear control techniques are developed and compared for the satellite attitude...
: We provide stabilizing and tracking feedback control laws for the kinematic system of an underactu...
The design of controllers subject to the nonlinear H-infinity criterion is explored. The plants to b...
In this paper, we deal with the attitude control of a satellite equipped with wheels of reaction, us...
Control of a class of uncertain nonlinear systems which can be decoupled by state-variable feedback ...
The attitude stabilization problem of a rigid spacecraft using control torques supplied by gas jet a...
A nonlinear control scheme for attitude control of a spacecraft is combined with a nonlinear gyro bi...
The paper deals with asymptotic tracking of a reference attitude trajectory for rigid spacecraft. Ba...
This article has adopted an analytical method to obtain a non-linear control law to reach the expone...
A control law is presented for asymptotic function reproducibility in a class of nonlinear-systems s...
A nonlinear adaptive control law for the attitude control of satellites using gyrotorquers is presen...
In this paper, we present a case study on spacecraft attitude control. The plant (spacecraft attitud...
In this paper two nonlinear control techniques are developed and compared for the satellite attitude...
A nonlinear control law for large angle rotational maneuvers of spacecraft using reaction wheels in ...
In this paper we consider the problem of controlling the orientation of a satellite with thrusters w...
In this paper two nonlinear control techniques are developed and compared for the satellite attitude...
: We provide stabilizing and tracking feedback control laws for the kinematic system of an underactu...
The design of controllers subject to the nonlinear H-infinity criterion is explored. The plants to b...
In this paper, we deal with the attitude control of a satellite equipped with wheels of reaction, us...
Control of a class of uncertain nonlinear systems which can be decoupled by state-variable feedback ...
The attitude stabilization problem of a rigid spacecraft using control torques supplied by gas jet a...
A nonlinear control scheme for attitude control of a spacecraft is combined with a nonlinear gyro bi...
The paper deals with asymptotic tracking of a reference attitude trajectory for rigid spacecraft. Ba...
This article has adopted an analytical method to obtain a non-linear control law to reach the expone...