DocumentCode :
2287811
Title :
GPS and INS flight test instrumentation of a fully aerobatic turbojet aircraft
Author :
Cutright, Curtis A. ; Braasch, Michael S.
Author_Institution :
Avionics Eng. Center, Ohio Univ., Athens, OH, USA
Volume :
3
fYear :
2002
fDate :
2002
Abstract :
This paper discusses the work performed at Ohio University to instrument its AERO Vodochody L-29 jet trainer. Simultaneous collection of Global Positioning System (GPS) and Inertial Navigation System (INS) data will allow researchers to perform a variety of flight test experiments and develop new applications. For example, real-time display of three-dimensional position would be extremely useful in aerobatic flight training (e.g., how circular is the loop you just performed). Given the typical drift rates of an INS, its sole use would be inappropriate. During inverted maneuvers (i.e., loops and rolls), however, GPS data will be lost for some time. The obvious answer is to integrate the GPS and INS. Although GPS/INS integration has been commonplace for quite some time, the aerobatic environment has only been addressed in military systems. Civilian flight training and aerobatic competitors could benefit from a commercially available GPS/INS that can provide high accuracy under extreme dynamics and inverted flight.
Keywords :
Global Positioning System; aircraft navigation; avionics; inertial navigation; AERO Vodochody L-29 jet trainer; GPS data; GPS flight test instrumentation; GPS/INS integration; Global Positioning System; INS data; INS flight test instrumentation; aerobatic flight training; aerobatic turbojet aircraft; aircraft system identification; civilian flight training; extreme dynamics; inertial navigation system; inverted flight; real-time display; three-dimensional position; Aerodynamics; Aerospace electronics; Aerospace engineering; Aircraft propulsion; Control systems; Global Positioning System; Instruments; Military aircraft; Testing; Vehicle dynamics;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference Proceedings, 2002. IEEE
Print_ISBN :
0-7803-7231-X
Type :
conf
DOI :
10.1109/AERO.2002.1035269
Filename :
1035269
Link To Document :
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