Add to ORKGAbstract: Collision avoidance approach for formation flying satellites in a Low Earth Orbit by aerodynamic drag is proposed. Energy optimal control to obtain tangent trajectory to forbidden zone is developed. A piecewise-linear approximation of optimal control is considered. Comparison of the two algorithms in terms of accuracy is performed. The accuracy of the control in the presence of discrete control and command execution error is studied.Note: Research direction:Theoretical and applied problems of mechanic
This thesis addresses the problems of orbit and attitude control for satellite formation flying. ...
A collision-free formation reconfiguration trajectory subject to the linearized Hill’s dynamics of r...
Propulsion, path planning and control of satellite formations in Geostationary Earth Orbits (GEO) an...
Abstract: Formation flying relative motion control in a Low Earth Orbit by aerodynamic dra...
According to later reports there are more than 18000 artificial satellites in space, with more than ...
The concept of the satellite formation flight is area where it is actively study with expandability ...
Abstract: Control of group of satellites in Low-Earth orbit by aerodynamic force is consid...
Abstract. In this paper we present a study on the Collision-Avoidance mode of a formation flying sa...
This paper proposes a linear system control algorithm with collision avoidance in multiple satellite...
This study investigates the use of a linear quadratic terminal controller to recon-figure satellite ...
Air drag can be used in very low Earth orbit to reliably generate moderate orbital control action wi...
Collision avoidance is more and more of importance due to the growing amount of space debris posing ...
Satellites flying in close proximity can provide many advantages over a single monolithic system.How...
Abstract: The paper discusses the problem of formation flying relative motion control by a...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76539/1/AIAA-16812-804.pd
This thesis addresses the problems of orbit and attitude control for satellite formation flying. ...
A collision-free formation reconfiguration trajectory subject to the linearized Hill’s dynamics of r...
Propulsion, path planning and control of satellite formations in Geostationary Earth Orbits (GEO) an...
Abstract: Formation flying relative motion control in a Low Earth Orbit by aerodynamic dra...
According to later reports there are more than 18000 artificial satellites in space, with more than ...
The concept of the satellite formation flight is area where it is actively study with expandability ...
Abstract: Control of group of satellites in Low-Earth orbit by aerodynamic force is consid...
Abstract. In this paper we present a study on the Collision-Avoidance mode of a formation flying sa...
This paper proposes a linear system control algorithm with collision avoidance in multiple satellite...
This study investigates the use of a linear quadratic terminal controller to recon-figure satellite ...
Air drag can be used in very low Earth orbit to reliably generate moderate orbital control action wi...
Collision avoidance is more and more of importance due to the growing amount of space debris posing ...
Satellites flying in close proximity can provide many advantages over a single monolithic system.How...
Abstract: The paper discusses the problem of formation flying relative motion control by a...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76539/1/AIAA-16812-804.pd
This thesis addresses the problems of orbit and attitude control for satellite formation flying. ...
A collision-free formation reconfiguration trajectory subject to the linearized Hill’s dynamics of r...
Propulsion, path planning and control of satellite formations in Geostationary Earth Orbits (GEO) an...