In this paper, the model-free formation control problem is addressed for multiple satellites, whose dynamics involves rotation-translation coupling and nonlinearities. A two-step adaptive control strategy is proposed based on the reinforcement learning theory to iteratively solve the optimal formation control problem without knowledge of each satellite dynamics. The resulted controller is composed of an attitude controller to achieve the desired attitude, and a relative position controller to construct the satellite formation. The proposed global closed-loop control system is proven to be asymptotically stable. Simulation results on rotation-translation coupled satellite system confirm the effectiveness of the proposed adaptive optimal form...
Autonomous control greatly reduces the demand on ground-based resources to keep satellites in a cons...
The inclusion of the linearized J2 effect in the Hill equations of relative motion gives greater in...
An innovative dynamics and control algorithm is developed for a dual-nanosatellite formation flying ...
In this paper, the model-free formation control problem is addressed for multiple satellites, whose ...
In this paper, a new universal adaptive control scheme for satellite formation flying is developed. ...
This thesis addresses the problems of orbit and attitude control for satellite formation flying. ...
Satellite formations or distributed satellite systems provide advantages not feasible with single sa...
Em publicação.We study the problem of formation shape control under the constraints on the thrust d...
Formation flying is a new paradigm in space mission design, aimed at replacing large satellites wit...
This paper addresses the problem of robust formation controller design for a group of satellites the...
The paper presents a new a new adaptive output feedback satellite formation control system for satel...
In this thesis we consider the problem of developing distributed control strategies for spacecraft f...
In recent years space missions for both scientific and commercial purposes have substantially increa...
The spacecraft formation control problem sets high demands to the performance, especially with respe...
This paper investigates the problem of rotating formation control for multi-spacecraft systems with ...
Autonomous control greatly reduces the demand on ground-based resources to keep satellites in a cons...
The inclusion of the linearized J2 effect in the Hill equations of relative motion gives greater in...
An innovative dynamics and control algorithm is developed for a dual-nanosatellite formation flying ...
In this paper, the model-free formation control problem is addressed for multiple satellites, whose ...
In this paper, a new universal adaptive control scheme for satellite formation flying is developed. ...
This thesis addresses the problems of orbit and attitude control for satellite formation flying. ...
Satellite formations or distributed satellite systems provide advantages not feasible with single sa...
Em publicação.We study the problem of formation shape control under the constraints on the thrust d...
Formation flying is a new paradigm in space mission design, aimed at replacing large satellites wit...
This paper addresses the problem of robust formation controller design for a group of satellites the...
The paper presents a new a new adaptive output feedback satellite formation control system for satel...
In this thesis we consider the problem of developing distributed control strategies for spacecraft f...
In recent years space missions for both scientific and commercial purposes have substantially increa...
The spacecraft formation control problem sets high demands to the performance, especially with respe...
This paper investigates the problem of rotating formation control for multi-spacecraft systems with ...
Autonomous control greatly reduces the demand on ground-based resources to keep satellites in a cons...
The inclusion of the linearized J2 effect in the Hill equations of relative motion gives greater in...
An innovative dynamics and control algorithm is developed for a dual-nanosatellite formation flying ...