The On-Orbit Autonomous Assembly from Nanosatellites (OAAN) project will demonstrate autonomous control algorithms for rendezvous and docking maneuvers; low-power reconfigurable magnetic docking technology; and compact, lightweight and inexpensive precision relative navigation using carrier-phase differential (CD) GPS with a three-degree of freedom ground demonstration. CDGPS is a specific relative position determination method that measures the phase of the GPS carrier wave to yield relative position data accurate to.4 inch (1 centimeter). CDGPS is a technology commonly found in the surveying industry. The development and demonstration of these technologies will fill a current gap in the availability of proven autonomous rendezvous and doc...
This paper presents a novel, GPS-based attitude determination system (ADS). Carrier-phase differenti...
Future space telescopes with diameter over 20 m will require new approaches: either high-precision f...
This paper describes the development of a three axis attitude control system for nanosatellites and ...
Small spacecraft autonomous rendezvous and docking (ARD) is an essential technology for future space...
Small spacecraft autonomous rendezvous and docking is an essential technology for future space struc...
Formation flying will quickly revolutionize the way science, remote sensing and surveillance mission...
Nanosatellite rendezvous missions can enable diagnostics and servicing of disabled spacecraft on a m...
A great deal of attention has been paid to navigation during the close approach (less than or equal ...
A revolution in spacecraft guidance, navigation and control technology has started with GPS to auton...
Future space telescopes with diameter over 20 m will require new approaches: either high-precision f...
Is it possible to dock CubeSats in Low Earth Orbit? The challenges are mainly associated with the le...
Project objectives The proposed research is part of a national project (coordinated by the Universit...
Enabling technologies for nanosatellite formations will be demonstrated under the Formation Autonomy...
Abstract A revolution in spacecraft guidance, navigation and control technology has started with GPS...
Future space telescopes with diameter over 20 m will require new approaches: either high-precision f...
This paper presents a novel, GPS-based attitude determination system (ADS). Carrier-phase differenti...
Future space telescopes with diameter over 20 m will require new approaches: either high-precision f...
This paper describes the development of a three axis attitude control system for nanosatellites and ...
Small spacecraft autonomous rendezvous and docking (ARD) is an essential technology for future space...
Small spacecraft autonomous rendezvous and docking is an essential technology for future space struc...
Formation flying will quickly revolutionize the way science, remote sensing and surveillance mission...
Nanosatellite rendezvous missions can enable diagnostics and servicing of disabled spacecraft on a m...
A great deal of attention has been paid to navigation during the close approach (less than or equal ...
A revolution in spacecraft guidance, navigation and control technology has started with GPS to auton...
Future space telescopes with diameter over 20 m will require new approaches: either high-precision f...
Is it possible to dock CubeSats in Low Earth Orbit? The challenges are mainly associated with the le...
Project objectives The proposed research is part of a national project (coordinated by the Universit...
Enabling technologies for nanosatellite formations will be demonstrated under the Formation Autonomy...
Abstract A revolution in spacecraft guidance, navigation and control technology has started with GPS...
Future space telescopes with diameter over 20 m will require new approaches: either high-precision f...
This paper presents a novel, GPS-based attitude determination system (ADS). Carrier-phase differenti...
Future space telescopes with diameter over 20 m will require new approaches: either high-precision f...
This paper describes the development of a three axis attitude control system for nanosatellites and ...