Asymmetrical spin stabilized satellite dynamics in the vicinity of the required motion is
considered. The principal axis of the maximum moment of inertia slightly deviates from its …

In this paper, a gyrostat satellite in a circular orbit with its gyrostatic moment tangent to the
orbital plane and collinear with the orbital speed is studied regarding its equilibria …

Because one-shot launch locking/unlocking device (OSLLUD) cannot repeat
locking/unlocking, and repeatable launch locking/unlocking device (RLLUD) has an …

A novel technique has been designed that creates rapid nutation damping and accurate
spin rate control for a spacecraft with arbitrary inertia ratio. In this approach the satellite …

This paper focuses upon the novel optical conical scanning imaging working mode design
for small satellites. This kind of satellite employs only one inclined optical camera achieving …

We consider the problem of tracking arbitrary free nutating trajectories of the Lagrange top
using linear feedback. The equations of motion of the top are linearised about the desired …

To solve the problem of thrust vector misalignment from the Cubesat center of mass during
orbital maneuver, spin-stabilized method is applied to eliminate velocity pointing error …

Magnetically suspended control and sensitive gyroscope (MSCSG) with two capabilities
including attitude control and attitude measurement is promising in meeting the …

This research relies on nutation control strategy through state feedback with its application to
a spin-stabilized autonomous system such as spacecraft. The key subject behind the …

This paper focuses on a single-axis control of a wheeled spin satellite while the entire
angular momentum is not zero. The presented technique includes a feedback control law …