The renewed interest on ducted rockets impulses their investigation. In this article, switching
control in the working process of ducted rockets is focused on, in order to obtain optimal …

This paper addresses the problem of integrated fault reconstruction and fault-tolerant control
in linear systems subject to actuator faults via learning observers (LOs). A reconfigurable …

Purpose The purpose of this paper is to accomplish robust actuator fault isolation and
identification for microsatellite attitude control systems (ACSs) subject to a series of space …

It is challenging to precisely control the attitude of a satellite when performing a fast and
large-angle maneuver, for instance, in the staring mode. To solve this issue, this paper …

The increase of satellite's dimensions has caused flexibility and formation of uncertainty in
their model. This is because of space missions being more complex and using light moving …

For the appearance of the additive perturbation of controller gain when the controller
parameter has minute adjustment at the initial running stage of system, to avoid the adverse …

This paper addresses the robust control problem of spacecraft body-fixed hovering near a
noncooperative target in the presence of parametric uncertainties and disturbances. A …

The problem of optimal synthesis of a nonlinear system's control law parameters of satellite
attitude control under constraints is considered. The maximum stability degree of a system is …

Three axes attitude control of CNES microsatellite is considered. The satellite has uncertain
inertia, natural frequency and damping. Satellite dynamics are modelized using descriptor …

This paper investigates the guaranteed cost attitude control problem of a rigid-body subject
to parameter uncertainty problem. The traditional LQR and guaranteed cost control (GCC) …