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dc.contributor.advisorJames K. Kuchar and John E. Keesee.en_US
dc.contributor.authorWolf, Travis Benjaminen_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2010-04-26T19:40:31Z
dc.date.available2010-04-26T19:40:31Z
dc.date.copyright2009en_US
dc.date.issued2009en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/54226
dc.descriptionThesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2009.en_US
dc.descriptionThis electronic version was submitted by the student author. The certified thesis is available in the Institute Archives and Special Collections.en_US
dc.descriptionCataloged from student submitted PDF version of thesis.en_US
dc.descriptionIncludes bibliographical references (p. 93-95).en_US
dc.description.abstractThis thesis presents the Monte Carlo Real-Time Belief Space Search (MC-RTBSS) algorithm, a novel, online planning algorithm for partially observable Markov decision processes (POMDPs). MC-RTBSS combines a sample-based belief state representation with a branch and bound pruning method to search through the belief space for the optimal policy. The algorithm is applied to the problem of aircraft collision avoidance and its performance is compared to the Trac Alert and Collision Avoidance System (TCAS) in simulated encounter scenarios. The simulations are generated using an encounter model formulated as a dynamic Bayesian network that is based on radar feeds covering U.S. airspace. MC-RTBSS leverages statistical information from the airspace model to predict future intruder behavior and inform its maneuvers. Use of the POMDP formulation permits the inclusion of different sensor suites and aircraft dynamic models. The behavior of MC-RTBSS is demonstrated using encounters generated from an airspace model and comparing the results to TCAS simulation results. In the simulations, both MC-RTBSS and TCAS measure intruder range, bearing, and relative altitude with the same noise parameters. Increasing the penalty of a Near Mid-Air Collision (NMAC) in the MC-RTBSS reward function reduces the number of NMACs, although the algorithm is limited by the number of particles used for belief state projections. Increasing the number of particles and observations used during belief state projection increases performance.en_US
dc.description.abstract(cont.) Increasing these parameter values also increases computation time, which needs to be mitigated using a more efficient implementation of MC-RTBSS to permit real-time use.en_US
dc.description.statementofresponsibilityby Travis Benjamin Wolf.en_US
dc.format.extent95 p.en_US
dc.language.isoengen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsM.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.rights.urihttp://dspace.mit.edu/handle/1721.1/7582en_US
dc.subjectAeronautics and Astronautics.en_US
dc.titleAircraft collision avoidance using Monte Carlo Real-Time Belief Space Searchen_US
dc.typeThesisen_US
dc.description.degreeS.M.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc601707491en_US


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