1. 1 INS Data Collection System For the Quarterly Review of the NASA/FAA Joint University Program for Air Transportation Research Wednesday October 10 th, 2001 Presented By: Jansen Litter Principal Investigator: Dr. Michael Braasch Avionics Engineering Center Ohio University, Athens Project Sponsor: Joint University Program

2. 2 Purpose Application of integrated GPS/INS to high dynamic vehicles Software development and modification are the primary focus at this time Initial hardware has been installed

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

4. 4 Delphin Cockpit

5. 5 Data Collection System Block Diagram 115V / 400Hz Air Data Computer Inertial Reference System PC-104 -Ethernet -ARINC Interface -Power Supply 28VDC ARINC 429 Bus 28VDC Power/Mode Selector Baro Set Corrections

6. 6 Data Collection INS data will be collected on the PC-104 computer through the ARINC card Time tagging will be accomplished using the CPU clock GPS data collection software will be added later

7. 7 Software Development ARINC card has four channels with both high and low speed capability Initialization data is transmitted in 2 to 4 bursts on the low speed bus INS data is received on the high speed bus

8. 8 Software Development (continued) Labels can be used to mask unwanted outputs Software can utilize three high speed buses on INS unit to receive data. Up to three programs can run simultaneously collecting data from INS unit

9. 9 Current Software Allows INS data collection Eventually allow INS-GPS data collection followed by INS-INS-GPS collection Data collected from multiple inputs will have a synchronous time tag to allow for comparison

10. 10 10 Software Modules Software written in modular format Modules initialize hardware and software »Initialize ARINC Card »Initialize INS Unit »Initialize CEI-400 »Initialize Time Stamp Code »Collect data from INS unit »Call all functions from main

11. 11 11 Hardware Configuration Encoding altimeter will be replaced with a variable potentiometer Control Display Unit (CDU) will be replaced with a single pole single throw switch

12. 12 12 PC-104 PC-104 handle(seen in center of picture)

13. 13 13 Mounting Rack Mounting rack for INS unit.

14. 14 14 Conclusions Software will change to meet goals of project Additional hardware will be integrated into the system sparking the evolution of the software

15. 15 Contact Information Principle Investigator:Dr. Michael Braasch braaschm@ohiou.edu Research Engineer:Curtis Cutright cutright@ieee.org Research Associate:Jansen Litter jansenlitter@ieee.org

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