Show simple item record

dc.contributor.advisorLaurence R. Young.en_US
dc.contributor.authorTritchler, Stephanie E. (Stephanie Elaine)en_US
dc.contributor.otherMassachusetts Institute of Technology. Department of Aeronautics and Astronautics.en_US
dc.date.accessioned2013-11-18T21:46:54Z
dc.date.available2013-11-18T21:46:54Z
dc.date.copyright2013en_US
dc.date.issued2013en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/82508
dc.descriptionThesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2013.en_US
dc.descriptionThis thesis was scanned as part of an electronic thesis pilot project.en_US
dc.descriptionCataloged from PDF version of thesis.en_US
dc.descriptionIncludes bibliographical references (p. 97-98).en_US
dc.description.abstractLanding is a dangerous and complex phase of any flight. Landing on an airless, dusty world presents unique challenges to perception, including dust blowback. During crewed lunar landings, astronauts will either be directly piloting the lander or supervising the automation in the event they need to take over piloting duties. An accurate perception of vehicle attitude is critical if the astronaut is to bring the craft down safely. We aim to study human perception of orientation under different visual cues using a helicopter simulator. We conducted a simulator-only lunar landing experiment with seventeen helicopter pilot subjects at USAARL utilizing the 6 degree-of-freedom moving-base UH-60 helicopter simulator. The subjects did not fly the simulator but continuously indicated his/her perceived pitch and roll angles throughout each trial by keeping a modified joystick aligned with Earth vertical, and the accuracy of the responses has been analyzed to determine the effect of visual cue on attitude perception. The subjects experienced recorded trajectories under five different visual conditions: no visual cues, out-the-window cues with no, medium, and high dust, and instrument cues. Regression models were fit to the correlations between the Subjects' indicated perceived pitch and roll angles and the simulator model pitch and roll angles. It was found that the no vision cue severely hindered the subjects' ability to accurately perceive craft attitude, while the instrument cue enhanced it. The effect of the different levels of dust, as compared to out-the-window no dust condition and the instrument conditions were not statistically significant, though they were better than no vision.en_US
dc.description.statementofresponsibilityby Stephanie E. Tritchler.en_US
dc.format.extent150 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.titleThe effect of dust blowback on spatial orientation estimation during lunar landingen_US
dc.typeThesisen_US
dc.description.degreeS.M.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc862456188en_US


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record