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STATIC AND DYNAMIC EVALUATION OF A GPS ATTITUDE DETERMINATION SYSTEM BASED ON NON-DEDICATED GPS RECEIVERS

ITC/USA 2006 Conference Proceedings / The Forty-Second Annual International Telemetering Conference and Technical Exhibition / October 23-26, 2006 / Town and Country Resort & Convention Center, San Diego, California / For the final evaluation of a GPS attitude determination algorithm, it was determined its true
performance in terms of accuracy, reliability and dynamic response. To accomplish that, a flight
test campaign was carried out to validate the attitude determination algorithm. In this phase, the
measured aircraft attitude was compared to a reference attitude, to allow the determination of the
errors. The system was built using non-dedicated airborne GPS receivers, and a complete Flight
Tests Instrumentation (FTI) System. The flight test campaign was carried out at the Brazilian’s
Flight Test Group T-25C 1956 Basic Trainer aircraft. The performance and accuracy of the
system is demonstrated under static and dynamics tests profiles, which are fully compliant with
the Federal Aviation Administration (FAA) Advisory Circular (AC) 25-7A. Dynamic response of
the system is evaluated.

Identiferoai:union.ndltd.org:arizona.edu/oai:arizona.openrepository.com:10150/604233
Date10 1900
CreatorsLeite, Nelson Paiva Oliveira, Walter, Fernando
ContributorsCTA - Grupo Especial de Ensaios em Vôo, ITA - Divisão de Telecomunicações
PublisherInternational Foundation for Telemetering
Source SetsUniversity of Arizona
Languageen_US
Detected LanguageEnglish
Typetext, Proceedings
RightsCopyright © International Foundation for Telemetering
Relationhttp://www.telemetry.org/

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