|
Georgia Tech's Institutional Repository >
Georgia Tech Conferences >
Space Systems Engineering Conference >
Space Systems Engineering Conference (1st - Atlanta - 2005) >
SSEC05. Session D: Earth Spacecraft and Sensors >
Please use this identifier to cite or link to this item:
http://hdl.handle.net/1853/8036
|
| Title: | XSS-10 Mission Results and Lessons Learned |
| Authors: | Davis, Thomas M. Melanson, David Air Force Research Laboratory (Wright-Patterson Air Force Base, Ohio). Space Vehicles Directorate ATK Thiokol Inc. Georgia Institute of Technology. Space Systems Design Lab |
| Subjects : | XSS-10 space flight Satellite inspection operations Proximity operations Post mission analyses Micro-Satellite Technology Development Program Micro-satellite technologies Inspection of a resident space object Autonomous navigation |
| Issue Date: | 10-Nov-2005 |
| Publisher: | Georgia Institute of Technology |
| Series/Report no.: | SSEC05. Session D;GT-SSEC.D.3 |
| Abstract: | The Air Force Research Laboratory established the Micro-Satellite Technology Development Program
(XSS series of flight demonstrations) to leverage micro-satellite technologies with the aim of providing
solutions to Air Force future space mission capabilities. XSS-10 was the first in this series and was
intended to demonstrate key operational concepts and technologies relating to close-in satellite inspection
operations. The XSS-10 program began in December 1997 and launched from Cape Canaveral on 29
January 2003 attached to the second stage of a Delta II. Eleven orbits later the XSS-10 micro-sat ejected
from the orbiting Delta second stage and successfully completed a brief series of semi-autonomous
maneuver and inspection operations using the Delta second stage as the RSO. The mission objectives of
XSS-10 were to demonstrate autonomous navigation, proximity operations, and inspection of a Resident
Space Object (RSO). XSS-10, a 31 kilogram micro-satellite launched as a secondary on a Delta II
expendable launch vehicle carrying a GPS satellite. XSS-10 was equipped with a visible camera, a star
sensor, GPS receiver and a mini SGLS system, all specially built for this program. In addition, a visible
camera was also mounted on the second stage to observe the release of the microsatellite and observe its
maneuvers. The XSS-10 micro satellite was released from the Delta II second stage after the GPS satellite
was released. Operating autonomously, on a preplanned course, XSS-10 performed its mission of
navigating around the Delta II second stage. Autonomously navigating around the second stage, at
preplanned positions, the microsatellite took images of the second stage and sent them back in real time.
During these demonstrations, XSS-10 demonstrated responsive checkout of the microsatellite and all of
its subsystems, autonomous navigation on a preplanned course and a variety of algorithms and mission
operations that are critical for future mission operations. This paper will discuss the results of the mission
and post mission analysis of the XSS-10 space flight. |
| Description: | This conference features the work of authors from: Georgia Tech’s Space Systems Design Lab, Aerospace Systems Design Lab, School of Aerospace Engineering, Georgia Tech Research Institute; NASA’s Jet Propulsion Laboratory, Marshall Space Flight Center, Goddard Space Flight Center, Langley Research Center; and other aerospace industry and academic institutions |
| Type: | Presentation |
| URI: | http://hdl.handle.net/1853/8036 |
| Appears in Collections: | SSEC05. Session D: Earth Spacecraft and Sensors Space Systems Engineering Conference (1st - Atlanta - 2005)
|
Items in SMARTech are protected by copyright, with all rights reserved, unless otherwise indicated.
|