Relative navigation for formation flying of spacecraft /

The objective of this thesis is to develop an efficient and robust approach for relative navigation and attitude estimation of spacecraft flying in formation. The approach developed here uses information from a new optical sensor that provides a line of sight vector from the master spacecraft to the...

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Bibliographic Details
Main Author: Alonso, Roberto Jorge
Format: Thesis eBook
Language:English
Published: [Place of publication not identified] : [publisher not identified] ; 2001.
Subjects:
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Call Number: 2001 Thesis A453
 
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2001 Thesis A453 Available

Available Online

Holdings details from Available Online
Call Number: 2001 Thesis A453
 
Call Number Status Get It
2001 Thesis A453 Available