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dc.contributor.advisorDraper, C. E.
dc.contributor.authorYates, Alan H.
dc.contributor.authorSchneider, Raymond J.
dc.contributor.authorBlough, I. Kinter
dc.contributor.authorYates, Alan H.en_US
dc.contributor.authorSchneider, Raymond J.en_US
dc.contributor.authorBlough, I. Kinteren_US
dc.dateAugust 1946
dc.date.accessioned2012-03-14T17:52:54Z
dc.date.available2012-03-14T17:52:54Z
dc.date.issued1946-08
dc.identifier.urihttps://hdl.handle.net/10945/6504
dc.descriptionThis thesis document was issued under the authority of another institution, not NPS. At the time it was written, a copy was added to the NPS Library collection for reasons not now known. It has been included in the digital archive for its historical value to NPS. Not believed to be a CIVINS (Civilian Institutions) title.en_US
dc.description.abstractThis paper deals with the 2CH101 computer used in the Central Fire Station System as installed in the U.S. Army Air Force's heavy bomber, type B-29. Essentially, the computer consists of six servomechanisms which position gears, "waggle sticks", and finally four differential syncho-generators, the latter modifying signals sent from the sighting station for ballistic and land corrections developed within the computer and transmitting resultant gun orders to the firing station. In their report the authors have presented results of detailed tests on three of the servomechanism channels, the Range Input Channel, the Azimuth Input channel, and the Elevation Input channel. Tests were made from a transfer function viewpoint. Certain static sensitivities were measured. The Altitude and Airspeed Input channel and the Azimuth and Elevation-Total Correction channels were not tested in through detail since certain essential units of the system were not available. However, other pertinent information on these channels is presented insofar as experimental determination was possible. Briefly, the chief results and conclusions may be listed as follows: (1) The servomechanism channels are properly damped and stable but have a rather low resonant frequency; (2) maximum speed of follow-up in these channels, as listed by the driving motors, is too slow to handle modern, high-velocity problems; (3) solution time is relatively long, and is approximately proportional to the amount of total correction required; (4) the overall computer performance is limited by the connector or discontinuous type of servomechanism used. These function as proportional type servos, and as such have steady state velocity errors.en_US
dc.description.urihttp://archive.org/details/performancenalys109456504
dc.language.isoen_US
dc.language.isoen_USen_US
dc.rightsThis publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.en_US
dc.subject.lcshAeronauticsen_US
dc.titlePerformance analysis of certain components of fire control equipment for bombing aircraften_US
dc.typeThesisen_US
dc.contributor.corporateMassachusetts Institute of Technology
dc.contributor.departmentAeronautical Engineering
dc.description.serviceU.S. Navy (U.S.N.) authors.en_US
dc.identifier.oclcocm27064162en_US
etd.thesisdegree.nameM.S.en_US
etd.thesisdegree.levelMastersen_US
etd.thesisdegree.grantorMassachusetts Institute of Technologyen_US
etd.verifiedyesen_US


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