Uncertainty Characterization Of Orbital Debris

Show simple item record


dc.contributor Matusewicz , Jolanta en_US
dc.date.accessioned 2007 -08 -23T01 :56 :23Z
dc.date.accessioned 2011 -08 -24T21 :40 :05Z
dc.date.available 2007 -08 -23T01 :56 :23Z
dc.date.available 2011 -08 -24T21 :40 :05Z
dc.date.issued 2007 -08 -23T01 :56 :23Z
dc.date.submitted August 2006 en_US
dc.identifier.uri http : / /hdl .handle .net /10106 /259
dc.description.abstract The increase of orbital debris in the low Earth orbit is a concern for the space industry . Spacecraft and satellites are at risk of collision with orbital debris . Collisions can damage sensitive components or result in catastrophic failure . Organizations such as the United States Space Command are responsible for tracking orbital debris using ground based sensor sites located around the world . Orbit determination techniques are used to estimate the position and velocity of the orbit using range , azimuth , and elevation measurements obtained from the sensors . Nine sensors from the Space Surveillance Network are simulated to track a debris object in an International Space Station orbit . Perturbations due to a 4 X 4 complex gravity model and an exponential atmospheric model are included in the two -body orbital equations of motion force model . The nonlinear batch least squares and the continuous -discrete extended Kalman filter techniques are used to estimate the debris orbit . en_US
dc.language.iso EN en_US
dc.publisher Aerospace Engineering en_US
dc.title Uncertainty Characterization Of Orbital Debris en_US
dc.type M .S .E . en_US

Citation

Uncertainty Characterization Of Orbital Debris. Available electronically from http : / /hdl .handle .net /10106 /259 .

Files in this item

Files Size Format View

There are no files associated with this item.

This item appears in the following Collection(s)

Show simple item record

Search DSpace

Advanced Search

Browse