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Distribued estimation architectures and algorithms for formation flying spacecraft

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dc.contributor.advisor Jonathan P. How. en_US Mandić, Milan en_US
dc.contributor.other Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. en_US 2007-01-10T16:40:54Z 2007-01-10T16:40:54Z 2006 en_US 2006 en_US
dc.description Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2006. en_US
dc.description Includes bibliographical references (leaves 133-137). en_US
dc.description.abstract Future formation flying missions are being planned for fleets of spacecraft in MEO, GEO, and beyond where relative navigation using GPS will either be impossible or insufficient. To perform fleet estimation for these scenarios, local ranging devices on each vehicle are being considered to replace or augment the available GPS measurements. These estimation techniques need to be reliable, scalable, and robust. However, there are many challenges to implementing these estimation tasks. Previous research has shown that centralized architecture is not scalable, because the computational load increases much faster than the size of the fleet. On the other hand, decentralized architecture has exhibited synchronization problems, which may degrade its scalability. Hierarchic architectures were also created to address these problems. This thesis will compare centralized, decentralized, and hierarchic architectures against the metrics of accuracy, computational load, communication load, and synchronization. It will also briefly observe the performance of these architectures when there are communication delays. en_US
dc.description.abstract (cont.) It will examine the divergence issue with the EKF when this estimator is applied to a system with poor initial knowledge and with non-linear measurements with large differences in measurement noises. It will analyze different decentralized algorithms and identify the Schmidt-Kalman filter as the optimal algorithmic choice for decentralized architectures. It will also examine the measurement bias problem in the SPHERES project and provide an explanation for why proposed methods of solving the bias problem cannot succeed. Finally, the SPHERES beacon position calibration technique will be proposed as an effective way to make the SPHERES system more flexible to a change of testing environment. en_US
dc.description.statementofresponsibility by Milan Mandic. en_US
dc.format.extent 137 leaves en_US
dc.format.extent 5452475 bytes
dc.format.extent 5801225 bytes
dc.format.mimetype application/pdf
dc.format.mimetype application/pdf
dc.language.iso eng en_US
dc.publisher Massachusetts Institute of Technology en_US
dc.rights M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission. en_US
dc.subject Aeronautics and Astronautics. en_US
dc.title Distribued estimation architectures and algorithms for formation flying spacecraft en_US
dc.type Thesis en_US S.M. en_US
dc.contributor.department Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. en_US
dc.identifier.oclc 74277855 en_US

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