Navigation algorithms and observability analysis for formation flying missions

dc.contributor.advisorBishop, Robert H., 1957-en
dc.creatorHuxel, Paul Johnen
dc.date.accessioned2008-08-28T22:54:04Zen
dc.date.available2008-08-28T22:54:04Zen
dc.date.issued2006en
dc.description.abstractNavigation algorithms and the corresponding observability analysis for formation flying missions are developed. The methodology of the observability analysis relates the physical geometry of the observers, as well as the spacecraft formation, to several measures of system observability. Relationships between these observability measures and the state error covariance are then derived to provided estimated bounds or forecasts for the expected navigation accuracy. These methods range from conservative time-invariant analytic bounds to more representative numerical forecasts using common dilution of precision metrics. The research also examines the robustness of the extended Kalman filter when simultaneously processing inertial and relative range measurements. It has been shown that processing relative range measurements in conjunction with inertial range measurements can directly increase the accuracy of the inertial state estimate. However, it has also been shown that when there is relatively large uncertainty in the state estimate the addition of relative measurements can cause an otherwise convergent filter to diverge. This dissertation considers several methods for preventing this divergence, as well as an in-depth examination of second-order terms to explain the basis of the problem. In particular, to illustrate their potential significance, analytical bounds are derived for the second-order terms.
dc.description.departmentAerospace Engineeringen
dc.format.mediumelectronicen
dc.identifierb61298839en
dc.identifier.oclc72823472en
dc.identifier.urihttp://hdl.handle.net/2152/2534en
dc.language.isoengen
dc.rightsCopyright is held by the author. Presentation of this material on the Libraries' web site by University Libraries, The University of Texas at Austin was made possible under a limited license grant from the author who has retained all copyrights in the works.en
dc.subject.lcshNavigation (Astronautics)en
dc.subject.lcshObservers (Control theory)en
dc.subject.lcshKalman filteringen
dc.subject.lcshAlgorithmsen
dc.titleNavigation algorithms and observability analysis for formation flying missionsen
dc.type.genreThesisen
thesis.degree.departmentAerospace Engineering and Engineering Mechanicsen
thesis.degree.disciplineAerospace Engineeringen
thesis.degree.grantorThe University of Texas at Austinen
thesis.degree.levelDoctoralen
thesis.degree.nameDoctor of Philosophyen

Access full-text files

Original bundle

Now showing 1 - 1 of 1
Loading...
Thumbnail Image
Name:
huxelp19059.pdf
Size:
2.78 MB
Format:
Adobe Portable Document Format

License bundle

Now showing 1 - 1 of 1
No Thumbnail Available
Name:
license.txt
Size:
1.65 KB
Format:
Plain Text
Description: