Andere Kunden interessierten sich auch für
![Maneuver Estimation Model for Relative Orbit Determination]( "Maneuver Estimation Model for Relative Orbit Determination")
Maneuver Estimation Model for Relative Orbit Determination60,99 €![An Algorithm for Efficient Maximum Likelihood Estimation and Confidence Interval Determination in Nonlinear Estimation Problems]( "An Algorithm for Efficient Maximum Likelihood Estimation and Confidence Interval Determination in Nonlinear Estimation Problems")
An Algorithm for Efficient Maximum Likelihood Estimation and Confidence Interval Determination in Nonlinear Estimation Problems60,99 €![Orbit Estimation Algorithms for a Microsatellite Rendezvous with a Non-Cooperative Target]( "Orbit Estimation Algorithms for a Microsatellite Rendezvous with a Non-Cooperative Target")
Orbit Estimation Algorithms for a Microsatellite Rendezvous with a Non-Cooperative Target64,99 €![Orbit Maneuver for Responsive Coverage Using Electric Propulsion]( "Orbit Maneuver for Responsive Coverage Using Electric Propulsion")
Orbit Maneuver for Responsive Coverage Using Electric Propulsion60,99 €![Methods for Aiding Height Determination in Pseudolite-Based Reference Systems Using Batch Least-Squares Estimation]( "Methods for Aiding Height Determination in Pseudolite-Based Reference Systems Using Batch Least-Squares Estimation")
Methods for Aiding Height Determination in Pseudolite-Based Reference Systems Using Batch Least-Squares Estimation60,99 €![Data Sorting and Orbit Determination of Tethered Satellite Systems]( "Data Sorting and Orbit Determination of Tethered Satellite Systems")
Data Sorting and Orbit Determination of Tethered Satellite Systems63,99 €![Investigation of Aerobraking to Return the Space Maneuver Vehicle to Low Earth Orbit from Geotransfer Orbit]( "Investigation of Aerobraking to Return the Space Maneuver Vehicle to Low Earth Orbit from Geotransfer Orbit")
Investigation of Aerobraking to Return the Space Maneuver Vehicle to Low Earth Orbit from Geotransfer Orbit63,99 €
As an increasing number of geostationary satellites fill a limited number of orbital slots, collocation of satellites leads to a risk of close approach or misidentification. The ability to detect maneuvers made by these satellites using optical observations can help to prevent these problems. Such a model has already been created and tested using data from the Air Force Maui Optical and Supercomputing site.The goal of this research was to create a more robust model which would reduce the amount of data needed to make accurate maneuver estimations. The Clohessy-Wiltshire equations were used to model the relative motion of a geostationary satellite about its intended location and a nonlinear least squares algorithm was developed to estimate the satellite trajectories.
Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.
Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.