DOI
https://doi.org/10.25772/8T74-GX16
Defense Date
2010
Document Type
Thesis
Degree Name
Master of Science
Department
Engineering
First Advisor
Robert Klenke
Abstract
This thesis documents a research project in which an autonomous flight control system (FCS) was designed to control and navigate small, high-speed, unmanned, jet-turbine powered fixed-wing aircraft. The FCS was designed to allow the aircraft to maintain controlled flight, and return to a home location, without any operator intervention. The flight control computer was built with an FPGA, using a Microblaze soft-core microprocessor running the uClinux operating system. The configurable FPGA computing platform allowed flexibility for interfacing quickly with a wide range of sensors and control modules. A commercial inertial measurement unit was used for aircraft state estimation, and the flight control system was able to provide stability and precise flight-path control for multiple turbinepowered aircraft over the wide flight airspeed envelope these vehicles are capable of. In addition, the custom ground control station which provides an operator control interface for the FCS is discussed.
Rights
© The Author
Is Part Of
VCU University Archives
Is Part Of
VCU Theses and Dissertations
Date of Submission
December 2010