This paper considers the problem of attitude synchronization and formation keeping of two spacecrafts, with a leader. Attitudes of spacecrafts are not measured directly, instead control torques are determined from the line-of-sight (LOS) vectors between two spacecrafts, and another set of LOS vectors from a common leader. We provide distributed position and attitude control laws. Attitude control law is proposed to ensure that the two follower spacecrafts reach attitude consensus. A formation keeping position control law is also proposed so that desired distance between two follower spacecrafts and each spacecraft to the leader is achieved. Proposed position control law uses relative velocities and LOS vectors in the respective body frames ...
The attitude synchronizing of formation flying spacecrafts is an essential ingredient in almost all ...
We propose controllers for leader-follower attitude synchronization of spacecraft formations in the ...
A simple analytical approach for formation-keeping of satellites in the presence of both orbital and...
We consider coupled attitude and position control of two spacecraft where absolute attitudes are not...
This paper considers the problem of formation control of three spacecraft consisting of one leader a...
In this paper we propose a novel control law for achieving attitude alignment and formation keeping ...
This paper considers the problem of controlling relative attitude between two spacecrafts, so as to ...
Abstract — This paper studies formation control of an arbi-trary number of spacecraft based on a ser...
Abstract — Relative attitude formation control systems are developed for multiple spacecraft, based ...
Abstract — Relative attitude formation control systems are developed for multiple spacecraft, based ...
The coordination of the attitude among different spacecraft belonging to a multiple platform system ...
In this paper, we consider a distributed attitude alignment problem for a team of deep space formati...
Satellite technologies have progressed significantly in the last years from the early experiments ma...
The problem of coordination and control of multiple spacecraft (MS) moving in formation is considere...
Abstract — The problem of synchronized multiple spacecraft rotations is revisited in the context of ...
The attitude synchronizing of formation flying spacecrafts is an essential ingredient in almost all ...
We propose controllers for leader-follower attitude synchronization of spacecraft formations in the ...
A simple analytical approach for formation-keeping of satellites in the presence of both orbital and...
We consider coupled attitude and position control of two spacecraft where absolute attitudes are not...
This paper considers the problem of formation control of three spacecraft consisting of one leader a...
In this paper we propose a novel control law for achieving attitude alignment and formation keeping ...
This paper considers the problem of controlling relative attitude between two spacecrafts, so as to ...
Abstract — This paper studies formation control of an arbi-trary number of spacecraft based on a ser...
Abstract — Relative attitude formation control systems are developed for multiple spacecraft, based ...
Abstract — Relative attitude formation control systems are developed for multiple spacecraft, based ...
The coordination of the attitude among different spacecraft belonging to a multiple platform system ...
In this paper, we consider a distributed attitude alignment problem for a team of deep space formati...
Satellite technologies have progressed significantly in the last years from the early experiments ma...
The problem of coordination and control of multiple spacecraft (MS) moving in formation is considere...
Abstract — The problem of synchronized multiple spacecraft rotations is revisited in the context of ...
The attitude synchronizing of formation flying spacecrafts is an essential ingredient in almost all ...
We propose controllers for leader-follower attitude synchronization of spacecraft formations in the ...
A simple analytical approach for formation-keeping of satellites in the presence of both orbital and...