- About
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The Global ETD Search service is a free service for researchers
to find electronic theses and dissertations. This service is
provided by the
Networked Digital Library of Theses and Dissertations.
Our metadata is collected from universities around the world. If you manage a university/consortium/country archive and want to be added, details can be found on the NDLTD website.
Search results
Showing 41 to 50 of 52299 (0.066 seconds)| 41 |
Interval logic and modified labelled-net for system specificationand verification /Chiu, Ping-kuen, Peter. January 1985 (has links)
Thesis--M. Phil., University of Hong Kong, 1985.
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| 42 |
A MINIMAL SENSITIVITY DESIGN METHOD FOR CONTROL SYSTEMSHaberman, David, 1944- January 1977 (has links)
No description available.
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| 43 |
THEORETICAL FOUNDATIONS FOR ANALYSIS OF TELEOLOGICAL SYSTEMSPollin, Jack Murph, 1922- January 1969 (has links)
No description available.
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An observer and regulator for linear systems with pure and distributed delaysStuk, Stephen Paul 12 1900 (has links)
No description available.
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| 45 |
An industrial dynamics study of an electronic equipment companyLuedtke, Arthur 12 1900 (has links)
No description available.
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| 46 |
An investigation of two measures of linear system memoryJackson, William Elbert 08 1900 (has links)
No description available.
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| 47 |
A system dynamics overview of recruitment of minority students at the Georgia Institute of TechnologySamms, Gavin Andrew 08 1900 (has links)
No description available.
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| 48 |
Validation of system dynamics models with a sequential procedure involving multiple quantitative methodsBarlas, Yaman 05 1900 (has links)
No description available.
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| 49 |
A computational technique for identification of linear systemsGuffee, Clifford Overall 08 1900 (has links)
No description available.
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Simulation and Longitudinal System Identification For Small Fixed Wing UAVsMay, Morgan 21 April 2014 (has links)
Unmanned Aerial Vehicles (UAVs) are used in many fields such as construction surveying and farming. These aircraft are typically less than 75kg and can be as light as 1kg. Because of the small size of the aircraft, and the increasing interest in this field, research is conducted to both accurately simulate these aircraft and identify their aerodynamic parameters by means of a low-cost and easy to implement methods. The research presented in this thesis describes the development of a comprehensive UAV simulation. This simulation is aimed at developing and testing different system identification techniques on the longitudinal mode of the aircraft. Two identification methods are tested on the simulation. These identification techniques are then examined on flight test data of an actual aircraft. The methods work well on the simulation results; however, flight test were performed in unfavorable environmental conditions and did produced any useful results.
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