arc.itu.edu.tr Collaborative Intent Exchange Based Flight Management System with Airborne Collision Avoidance for UAS Emre Koyuncu*, Cengiz Pasaoglu**, Prof. Gokhan Inalhan* *Istanbul Technical University **DHMI, General Directorate Of State Airports Authority and Navigation Service Provider Turkey arc.itu.edu.tr
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Collaborative Intent Exchange Based Flight Management System with Airborne Collision
Avoidance for UAS Emre Koyuncu*, Cengiz Pasaoglu**, Prof. Gokhan Inalhan*
*Istanbul Technical University **DHMI, General Directorate Of State Airports Authority
and Navigation Service Provider Turkey
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arc.itu.edu.tr
INSTITUTONAL BACKGROUND
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Aeronautics Research Center
• Central Laboratory for Aeronautics Research (2012-) – +7 Faculty, 15 Research Associates, +20 Ph.D. Level
Researchers • Established to promote advanced, interdisciplinary and
experimental research • Research Focus on wide spectrum of Aeronautics
Technologies • Design of manned and unmanned air vehicles,
spacecraft and spacecraft systems • Air Transportation, ATM • Flight Controls, Simulation and Avionics, • Nanoengineered Composites • Engine technologies and combustion • Aerodynamics, Aeroelasticity
• Strong outreach at both university, national and international level
– Nanotechnologies and Material Sciences – Electronics and Computer Science
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Research Partners and Sponsors
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Controls and Avionics Laboratory • Research Focus
– Advanced flight controls and avionics technologies – Unmanned air vehicles design and autonomy – Air Transport and ATM – Spacecraft Systems Design – Data Analytic Modelling, Estimation, Control and
Learning • Notable Achievements
– Designed the first Turkish indigenous commercial avionics systems 2006-2009
– Designed and built the first Turkish university-level autopilot system for UAVs. 2006-2009
– Designed and built the first Turkish University picosat : ITUpSAT I (TUBITAK) 2006-2009
– Designed and built indigenous bus and ADCS components for nano and micro-satellites ITUpSAT II (TUBITAK 108M523) 2009-2012
– Winner of AIAA/AAS Cansat Picosat Competion 2011
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UAS RESEARCH
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TURAC : Environmental Monitoring UAV
TURAC Configuration
Wingspan 4.2 m
Total Length 1.8 m
Height 1.05 m
Front Propeller Diameter 0.43 m
Empty Weight 39 kg
Maximum Takeoff Weight 47 kg
Havelsan-ITU Project
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TURAC : Environmental Monitoring UAV
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TURAC : Environmental Monitoring UAV
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4D TRAJECTORY MANAGEMENT
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Flight Deck Automation Support with Dynamic 4D Trajectory Management
Short-Term Collision Avoidance – for midair and terrain collision Probabilistic (multi threat) midair and terrain collision monitoring
Fully automated flight control take-over implementation for delayed pilot response
Certifiable Pseudo-random/probabilistic algorithms with modal maneuver approach
Collaborative Tactical Planning – for dynamically changing environmental/operational conditions and use of airspace
Intent based collaborative decision making with the ATC (high level language – FIDL)
On-board tactical conflict monitoring and resolution via air/air link (low level language – AIDL)
Incorporating all tactical level information through air/ground data link + on-board sense