Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76446/1/AIAA-2000-4135-333.pd
We apply Floquet theory to the problem of designing a control system for a satellite in an unstable ...
There is an increasing interest in missions employing groups of satellites flying in formations and ...
This paper addresses the computation of the required trajectory correction maneuvers (TCM) for a ha...
This dissertation studies formation flight in the unstable environment about the Earth-Sun halo orbi...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76533/1/AIAA-8433-932.pd
[[abstract]]This paper investigates the potential control law that stabilizes relative trajectories ...
UnrestrictedSpacecraft formation flying involves operating multiple spacecraft in a pre-determined g...
Relative translational motion control, and motion stability between satellites in neighboring ellipt...
This paper presents rich new families of relative orbits for spacecraft formation ight generated thr...
The dynamics, stability, and control of a large family of non-Keplerian orbits are investigated and ...
The relative motion problem is analyzed, as a linearized case, and as a numerically determined solut...
The study of satellite relative motion has been of great historic interest, primarily due to its app...
The exploration of planetary satellites by robotic spacecraft is currently of strong scientific inte...
Paper given at Dynamics and Control of Systems and Structures in Space (DCSSS), 6th conference, Ri...
Near Rectilinear Halo Orbits (NRHOs) are stable or nearly stable orbits that are defined as part of ...
We apply Floquet theory to the problem of designing a control system for a satellite in an unstable ...
There is an increasing interest in missions employing groups of satellites flying in formations and ...
This paper addresses the computation of the required trajectory correction maneuvers (TCM) for a ha...
This dissertation studies formation flight in the unstable environment about the Earth-Sun halo orbi...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76533/1/AIAA-8433-932.pd
[[abstract]]This paper investigates the potential control law that stabilizes relative trajectories ...
UnrestrictedSpacecraft formation flying involves operating multiple spacecraft in a pre-determined g...
Relative translational motion control, and motion stability between satellites in neighboring ellipt...
This paper presents rich new families of relative orbits for spacecraft formation ight generated thr...
The dynamics, stability, and control of a large family of non-Keplerian orbits are investigated and ...
The relative motion problem is analyzed, as a linearized case, and as a numerically determined solut...
The study of satellite relative motion has been of great historic interest, primarily due to its app...
The exploration of planetary satellites by robotic spacecraft is currently of strong scientific inte...
Paper given at Dynamics and Control of Systems and Structures in Space (DCSSS), 6th conference, Ri...
Near Rectilinear Halo Orbits (NRHOs) are stable or nearly stable orbits that are defined as part of ...
We apply Floquet theory to the problem of designing a control system for a satellite in an unstable ...
There is an increasing interest in missions employing groups of satellites flying in formations and ...
This paper addresses the computation of the required trajectory correction maneuvers (TCM) for a ha...
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