This paper addresses the minimum-fuel spacecraft formation reconfiguration maneuver in J2 perturbed near-circular orbits. In this study, only the deputy is assumed to be maneuverable and capable of..
This thesis proposes a continuous low-thrust guidance and control strategy for satellite formation-f...
Satellites flying in close proximity can provide many advantages over a single monolithic system.How...
This paper presents the control solutions to the spacecraft formation reconfiguration problem when i...
This paper addresses the minimum-fuel spacecraft formation reconfiguration maneuver in J2 perturbed ...
This paper focuses on the fuel-minimum in-plane spacecraft reconfiguration ma-neuver in 2 perturbed ...
Advanced multisatellite missions based on formation-flying and on-orbit servicing concepts require t...
In this work both reconfiguration and station keeping maneuvers of spacecraft flying in formation wi...
In this work both reconfiguration and station keeping maneuvers of spacecraft flying in formation wi...
In this work the reconfiguration of spacecrafts flying in formation with low-thrust propulsion has b...
In this work the reconfiguration of spacecrafts flying in formation with low-thrust propulsion has b...
This paper presents the solutions to the spacecraft relative trajectory reconfiguration problem when...
Currently micro/nano satellites have become the protagonists in most formation flying missions, and ...
This thesis addresses the problems of orbit and attitude control for satellite formation flying. ...
This paper extends a previously developed method for finding spacecraft initial conditions (ICs) tha...
Formation flying of spacecraft has gained a lot of interest within the engineering and scientific co...
This thesis proposes a continuous low-thrust guidance and control strategy for satellite formation-f...
Satellites flying in close proximity can provide many advantages over a single monolithic system.How...
This paper presents the control solutions to the spacecraft formation reconfiguration problem when i...
This paper addresses the minimum-fuel spacecraft formation reconfiguration maneuver in J2 perturbed ...
This paper focuses on the fuel-minimum in-plane spacecraft reconfiguration ma-neuver in 2 perturbed ...
Advanced multisatellite missions based on formation-flying and on-orbit servicing concepts require t...
In this work both reconfiguration and station keeping maneuvers of spacecraft flying in formation wi...
In this work both reconfiguration and station keeping maneuvers of spacecraft flying in formation wi...
In this work the reconfiguration of spacecrafts flying in formation with low-thrust propulsion has b...
In this work the reconfiguration of spacecrafts flying in formation with low-thrust propulsion has b...
This paper presents the solutions to the spacecraft relative trajectory reconfiguration problem when...
Currently micro/nano satellites have become the protagonists in most formation flying missions, and ...
This thesis addresses the problems of orbit and attitude control for satellite formation flying. ...
This paper extends a previously developed method for finding spacecraft initial conditions (ICs) tha...
Formation flying of spacecraft has gained a lot of interest within the engineering and scientific co...
This thesis proposes a continuous low-thrust guidance and control strategy for satellite formation-f...
Satellites flying in close proximity can provide many advantages over a single monolithic system.How...
This paper presents the control solutions to the spacecraft formation reconfiguration problem when i...
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