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Analog computer study of an automatic landing system for aircraftBoyd, William P. January 1963 (has links)
Thesis (M.S.)--University of Wisconsin--Madison, 1963. / Typescript. eContent provider-neutral record in process. Description based on print version record. Includes bibliographical references (leaves [64]-65).
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Differential global positioning system for precision landingsNguyen, Tam Xuan. January 1990 (has links)
Thesis (M.S.)--Ohio University, August, 1990. / Title from PDF t.p.
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A comparative study of flare paths for aircraft automatic landing systemsGrzelak, Theodore Alan. January 1962 (has links)
Thesis (M.S.)--University of Wisconsin--Madison, 1962. / Typescript. eContent provider-neutral record in process. Description based on print version record. Includes bibliographical references (leaves [123]-125).
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Application of Airborne Laser Scanner - aerial navigationCampbell, Jacob L. January 2006 (has links)
Thesis (Ph.D.)--Ohio University, June, 2006. / Title from PDF t.p. Includes bibliographical references (p. 104-112)
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Development of siting criteria for the collocation of the microwave landing system (MLS) and the approach lighting system (ALS)Mathias, Sally A. January 1988 (has links)
Thesis (M.S.)--Ohio University, June, 1988. / Title from PDF t.p.
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Implementation of BMLS (baseline microwave landing system) computer model on hypercube processorsMylvaganam, Mohanaharan. January 1991 (has links)
Thesis (M.S.)--Ohio University, August, 1991. / Title from PDF t.p.
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DME/P critical area determination and its implementation on message-passing processorRajendran, Jaikishan. January 1992 (has links)
Thesis (M.S.)--Ohio University, November, 1992. / Title from PDF t.p.
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Accurate target geolocation and vision-based landing with application to search and engage missions for miniature air vehicles /Barber, D. Blake January 2007 (has links) (PDF)
Thesis (M.S.)--Brigham Young University. Dept. of Mechanical Engineering, 2007. / Includes bibliographical references (p. 93-96).
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An analysis of the static and dynamic characteristics of a decoupled landing entry vehicleHaile, James Ernest January 1968 (has links)
A theoretical analysis of the static and dynamic characteristics of an entry vehicle utilizing the decoupled landing concept has been conducted. A hypersonic arbitrary-body aerodynamic computer program was used to determine the aerodynamics of the basic body. Three theories were used and compared with data obtained for a Mach number equal to nineteen. Several stabilizing devices were investigated to determine which were the most effective in providing static stability. To evaluate the lateral-directional handling qualities, a ω<sub>Θ</sub>/ω<sub>d</sub> coupling parameter along with the parameter abs(Θ/β) were derived to be applicable during hypersonic entry. Equations were also derived for determining the contribution of the stabilizing devices to the dynamic stability derivatives. In the evaluation of the vehicle dynamic characteristics linearized equations of motion for the longitudinal and lateral directional modes were used at several points along a maximum performance trajectory. The parameters considered throughout the trajectory were the period and the time to damp to one-half amplitude. / Master of Science
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Analysis of error propagation in differential satellite based positioning systems /Krishnan, Vignesh. January 2004 (has links)
Thesis (M.S.)--Ohio University, August, 2004. / Includes bibliographical references (p. 84-87)
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