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In the fall of 2004, the High Speed Autonomous Vehicle Team, a group of 16 students took on the goal of converting a vehicle to drive-by-wire status. The main goal of this project was to convert a Cadillac SRX donated by General Motors, to fully by-wire control. This thesis presents the HSAVT brake-by-wire and the steer-by-wire solution. In addition, the results of a literary search on drive-by-wire systems are presented. The results of the project proved that the team came up with a solid, effective drive-by-wire vehicle and that the project met all of the primary goals of the project. / Master of Science

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No description available.

Thesis (M.S.)--State University of New York at Binghamton, Watson School of Engineering and Applied Science (Electrical Engineering), 2007. / Includes bibliographical references.

Thesis (M.S.)--University of Michigan, 1963.

Thesis (M.S.)--University of Michigan, 1963.

Thesis (M.S.)--University of Michigan, 1944.

Fly-by-wire flight control systems are becoming more common in both civil and military aircraft. These systems give many benefits, but also present a new set of problems due to their increased complexity compared to conventional systems and the larger choice of options that they provide. The work presented here considers the application of fly-by-wire to a generic regional transport aircraft. The flying qualities criteria used for typical flying qualities evaluations are described briefly followed by analysis of several past transport aircraft flying qualities programmes against these criteria. From these results, some control law independent design requirements are formulated for a civil aircraft for the approach and landing task. These control law independent flying qualities criteria are intended to be used with any generic rate-like control law for a transport aircraft and enabled a number of different control laws to be designed. The results of a number of flying qualities evaluations are presented. Both an ILS approach task and a formation flying task were used. The effects of windshear were also considered. It was found that control laws which maintain flight path are suitable for the ILS approach task, while most rate-like response characteristics give good flying qualities for the formation flying task. Finally, the conclusions drawn from these evaluations are presented, and both the Civil and Military current airworthiness requirements are assessed. In addition to the flying qualities work, a study is made of the management issues associated with fly-by-wire design. A fly-by-wire aircraft design programme was proposed and the project management issues associated with this were considered. A timescale was proposed for the design process for a generic regional aircraft, and the critical path for this process is presented.

No description available.