The success of the solution to the task of controlling the spacecraft's angular motion around
its centre of mass largely depends on the chosen model of the spacecraft's angular motion …

This paper proposes an optimal integral sliding mode control (ISMC) scheme for attitude
regulation of the rigid spacecraft. This control technique is capable of handling inertial matrix …

This paper proposes a robust event-driven control for attitude regulation in flexible
spacecraft affected by inertial parametric uncertainties and external disturbances. The …

This paper investigates the application of an integral sliding mode control with a robust
nonlinear disturbance observer to obtain an anti-unwinding spacecraft attitude tracking …

An optimal control scheme for attitude control of rigid body spacecraft is proposed in this
paper. The dynamic optimal control problem is first converted into a nonlinear programming …

In an age where minimization of resources is of prime importance, a control technique is
proposed in this paper which uses limited communication. The concept of event-trigger …

This paper aims at designing an energy-efficient state feedback control law for attitude
regulation of a rigid spacecraft system. The desired feedback control structure is achieved …

This paper proposes a control methodology for the attitude regulation of a rigid spacecraft
without the measurement knowledge of angular velocities and is affected by parametric …

Pathogen suppressing and immune boosting drugs, are used as control measure for
regulating the infections due to water borne disease. A mathematical SIWR (susceptible …

The regulation of satellite orientation in an orbit is an essential task for the success of a
space mission. To reorient the attitude of a satellite from an initial point to the desired …