Vehicle design, flight control avionics, and flight tests for the Parent and Child Unmanned Air Vehicle

The Parent and Child Unmanned Aerial Vehicle (PCUAV) is the second project to originate from the MIT / Draper Technology Development Partnership, which aims to develop first-of-a-kind systems. The PCUAV proposes a low-cost solution to long distance closeup observation, using the cooperative action of a fleet of small UAVs. The project team will prove the potential of the system by demonstrating key enablers such as autonomous air rendezvous. This thesis presents the design of the project's vehicles, namely the Mini and Parent vehicles, and the Avionics Testbed Airplane. The avionics architecture is discussed including a detailed description of its components and their selection. The approach to obtain reliable estimates of aircraft attitude using low-cost gyroscopes is introduced. The planning and execution of several flight tests is presented.

Department dc:contributor.department

Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.

Grantor dc:publisher

Massachusetts Institute of Technology

Year dc:date.issued

2001

Author dc:creator

• Urbain, Francois, 1974-

Advisor dc:contributor.advisor

• John J. Deyst, Jr. and James D. Paduano.

• Aeronautics and Astronautics.

Statement dc:rights

• M.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.

Licence dc:rights.uri

• http://dspace.mit.edu/handle/1721.1/7582

Language dc:language.iso

eng

Handle dc:identifier.uri

http://hdl.handle.net/1721.1/44900

OAI identifier oai:identifier

oai:dspace.mit.edu:1721.1/44900