Add to ORKGWe study the problem of orbital control under the constraints on the thrust direction for a nonlinear dynamical model. The satellite is equipped with a passive attitude control system providing one-axis stabilization and a propulsion system consisting of one or two thrusters oriented along the stabilized axis. Different applications, such as formation flying and satellite de-orbiting are considered.FC
2012-10-19This dissertation handles two topics that are fundamental in understanding aerospace and m...
In this paper, the problem of autonomous optimal absolute orbit keeping for a satellite mission in L...
The development of feedback control systems for autonomous orbital rendezvous is a key technological...
We study the problem of orbital control under the constraints on the thrust direction for a nonlinea...
Em publicação.We study the problem of formation shape control under the constraints on the thrust d...
peer reviewedThis paper provides a new, exact controller for formation-keeping in the presence of at...
This research is focused on the definition, analysis, and numerical testing an effective orbit contr...
113 p.Thesis (Ph.D.)--University of Illinois at Urbana-Champaign, 1985.Optimal open loop and nonline...
Regarding multiple spacecraft formation flying, the observation has been made that control thrust ne...
A simple analytical approach for formation-keeping of satellites in the presence of both orbital and...
A Newton-type method is proposed to improve the accuracy of control for relative motion of two satel...
In this paper we consider the problem of controlling the orientation of a satellite with thrusters w...
This thesis proposes a continuous low-thrust guidance and control strategy for satellite formation-f...
This thesis addresses the problems of orbit and attitude control for satellite formation flying. ...
Space research is currently in a trend of using smaller satellites in cooperation to achieve the s...
2012-10-19This dissertation handles two topics that are fundamental in understanding aerospace and m...
In this paper, the problem of autonomous optimal absolute orbit keeping for a satellite mission in L...
The development of feedback control systems for autonomous orbital rendezvous is a key technological...
We study the problem of orbital control under the constraints on the thrust direction for a nonlinea...
Em publicação.We study the problem of formation shape control under the constraints on the thrust d...
peer reviewedThis paper provides a new, exact controller for formation-keeping in the presence of at...
This research is focused on the definition, analysis, and numerical testing an effective orbit contr...
113 p.Thesis (Ph.D.)--University of Illinois at Urbana-Champaign, 1985.Optimal open loop and nonline...
Regarding multiple spacecraft formation flying, the observation has been made that control thrust ne...
A simple analytical approach for formation-keeping of satellites in the presence of both orbital and...
A Newton-type method is proposed to improve the accuracy of control for relative motion of two satel...
In this paper we consider the problem of controlling the orientation of a satellite with thrusters w...
This thesis proposes a continuous low-thrust guidance and control strategy for satellite formation-f...
This thesis addresses the problems of orbit and attitude control for satellite formation flying. ...
Space research is currently in a trend of using smaller satellites in cooperation to achieve the s...
2012-10-19This dissertation handles two topics that are fundamental in understanding aerospace and m...
In this paper, the problem of autonomous optimal absolute orbit keeping for a satellite mission in L...
The development of feedback control systems for autonomous orbital rendezvous is a key technological...