1. 1 GPS/INS Flight Testing on the L-29 Delfin For the Quarterly Review of the Joint University Program for Air Transportation Research Friday, October 18 th, 2002 Curtis Cutright, Jansen Litter, Dan Suriyamongkol, Michael S. Braasch Avionics Engineering Center Ohio University, Athens

2. 2 Purpose Hardware/software sensor testbed Software INS/GPS integration Noise versus dynamic tracking error trade off Synthetic aperture radar Aircraft system id/flight control design educational tool

3. 3 Flight Test Vehicle L - 29 Delfin High Altitude 11 Km High Speed 354 knots Fully Aerobatic Flight Specs Taken From http://aeroweb.brooklyn.cuny.edu/specs/aero/l-29.htm

4. 4 Delphin Equipment Navigation Grade INS Industrial Keyboard Shock-hardened Computer Industrial Flat Panel Display NovAtel GPS Receiver Navigation Grade IMU

5. 5 Project Development Initial equipment installation is complete GPS and INS data collected simultaneously in real time Previous INS problem solved: the unit needed to know whether it was in the left, center or right position (the unit was designed to be part of a triple-redundant installation)

6. 6 System Block Schematic ADCINS PC104 GPS data 12 VDC Aircraft Power 28 VDC INV 115VAC/ 400Hz Potentiometer data Power Data

7. 7 Installed Equipment ADCInverter

8. 8

9. 9 Installed Equipment Continued Industrial Keyboard INS On Switch

10. 10 10 Installed Equipment Continued Novatel GPS ReceiverControl Switches

11. 11 11 Installed Equipment Continued GPS Antenna

12. 12 12 Flight Test – July 17, 2002

13. 13 13 GPS and INS-Derived Profiles

14. 14 14 GPS-Derived Height

15. 15 15 GPS-Derived Ground Speed

16. 16 16 GPS/INS Latitude Difference

17. 17 17 GPS/INS Longitude Difference

18. 18 18 GPS/INS Horizontal Difference

19. 19 19 GPS & INS Position Resolution

20. 20 20 Conclusions Difficult to collect high-rate data from multiple sensors with a single PC Currently investigating alternative data collection strategies; leaning toward installation of a 2 nd PC- 104 Will be working with Frank van Graas to flight test high accuracy GPS velocity determination algorithms (principle application: Synthetic Aperture Radar)

21. 21 21 Contact Information Principle Investigator:Dr. Michael Braasch Braaschm@ohiou.edu Research Engineer:Curtis Cutright Cutright@ieee.org