This paper proposes an optimal control method for the chaotic attitude of the satellite when it
is exposed to external disturbances. When there is no control over the satellite, its chaotic …

Recently, there has been signifficant development in the existence of mild solutions for
fractional semilinear integro-differential equations but optimal control is not provided. The …

In this paper, a finite-time control scheme is presented for stabilization of the satellite chaotic
attitude around its equilibrium point when its attitude is confused by a disturbed torque …

The increase in demand for performance for satellite capabilities has pushed the design of
the system to be more power consuming. Currently, most of the satellite design are …

This article uses impulsive control along with quaternion parameters instead of Euler angles
in kinematics equations of satellite. The quaternion parameters are applied to overcome …

Reaction wheel is the most popular actuator for the attitude manoeuvring of a satellite
system due to its compact size, reliability and able to produce precise torque. However, for …

This article uses impulsive control along with quaternion parameters instead of Euler angles
in kinematics equations of satellite. ‎ The quaternion parameters are applied to …

Recently, there has been significant development in the existence of mild solutions for
fractional semilinear integro-differential equations but optimal control is not provided. The …