Title:
System Integration and Operation of a Research Unmanned Aerial Vehicle

dc.contributor.author Johnson, Eric N.
dc.contributor.author Schrage, Daniel P.
dc.contributor.corporatename Georgia Institute of Technology. School of Aerospace Engineering
dc.date.accessioned 2011-02-15T18:04:36Z
dc.date.available 2011-02-15T18:04:36Z
dc.date.issued 2004-01
dc.description.abstract The use of flight simulation tools to reduce the schedule, risk, and required amount of flight-testing for complex aerospace systems is a well-recognized benefit of these approaches. However, some special challenges arise when one attempts to obtain these benefits for the development and operation of a research Uninhabited Aerial Vehicle (UAV) system. Research UAV systems are characterized by the need for continual checkout of experimental software and hardware. Also, flight-testing can be further leveraged by complementing experimental results with flight-test validated simulation results for the same vehicle system. In this paper, flight simulation architectures for system design, integration, and operation of an experimental helicopter-based UAV, are described. The chosen helicopter-based UAV platform (a Yamaha RMax) is well instrumented: differential GPS, an inertial measurement unit, sonar altimetry, and a 3-axis magnetometer. One or two general-purpose flight processors can be utilized. Research flight test results obtained to date, including those completed in conjunction with the DARPA Software Enabled Control program, are summarized. en_US
dc.identifier.citation System Integration and Operation of a Research Unmanned Aerial Vehicle. Eric N. Johnson, Daniel P. Schrage. Journal of Aerospace Computing, Information, and Communication, 1(1):5-18, January, 2004. en_US
dc.identifier.issn 1542-9423
dc.identifier.uri http://hdl.handle.net/1853/36909
dc.language.iso en_US en_US
dc.publisher Georgia Institute of Technology en_US
dc.publisher.original American Institute of Aeronautics and Astronautics
dc.subject Flight simulators en_US
dc.subject Flight tests en_US
dc.title System Integration and Operation of a Research Unmanned Aerial Vehicle en_US
dc.type Text
dc.type.genre Post-print
dspace.entity.type Publication
local.contributor.author Johnson, Eric N.
local.contributor.corporatename Unmanned Aerial Vehicle Research Facility
relation.isAuthorOfPublication 175a1f2b-c14e-4c43-a9e5-136fb7f8e5d0
relation.isOrgUnitOfPublication 5a379df1-c9ee-4bc9-a46e-9969e0eda2b1
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