Keynote Speakers
(Names sorted in alphabetical order)
Openning Keynote Speakers
Maximillian Platzer
Lifetime Honorary President of SARES, USA
Presentation Title: Title
Title
Lorem ipsum dolor sit amet, consectetur adipiscing elit. Ut elit tellus, luctus nec ullamcorper mattis, pulvinar dapibus leo.
Lorem ipsum dolor sit amet, consectetur adipiscing elit. Ut elit tellus, luctus nec ullamcorper mattis, pulvinar dapibus leo.
- Interest-1
- Interest-2
- Interest-3
- Interest-4
- Interest-5
T. Hikmet Karakoç
Director of Research and Application Center of Civil Aviation, Eskişehir Technical University, Türkiye
Presentation Title: Title
Title
Lorem ipsum dolor sit amet, consectetur adipiscing elit. Ut elit tellus, luctus nec ullamcorper mattis, pulvinar dapibus leo.
Lorem ipsum dolor sit amet, consectetur adipiscing elit. Ut elit tellus, luctus nec ullamcorper mattis, pulvinar dapibus leo.
- Interest-1
- Interest-2
- Interest-3
- Interest-4
- Interest-5
Keynote Speakers
Chingiz Hajiyev
Istanbul Technical University, Türkiye
Presentation Title: Relative Navigation of LEO Satellites in Formation Using Probabilistic Adaptive EKF
Relative Navigation of LEO Satellites in Formation Using Probabilistic Adaptive EKF
In this study, a new approach for autonomous relative navigation for two low Earth Orbit (LEO) satellite formations based on Global Navigation Satellite System (GNSS) measurements is presented. The method utilizes nonlinear GNSS data and Keplerian orbit parameters to estimate the states of both the primary and slave satellites using the proposed Probabilistic Adaptive Extended Kalman Filters (pAEKFs). Furthermore, this approach integrates the state vectors generated by pAEKFs using the Hill-Clohessy-Wiltshire (HCW) relative motion model to improve the accuracy of the relative state estimation between the satellites. A traditional Kalman filter without the adaptation procedure is proposed to estimate the parameters of the Hill-Clohessy-Wiltshire relative motion model. This strategy aims to improve the robustness and accuracy of the satellite formation control in LEO operations.
Prof.Dr. Chingiz Hajiyev, graduated from Moscow Aviation Institute, Moscow, Russia, with honors in 1981. He received his Ph.D. and DSc (Eng) degrees in Process Control in 1987 and 1993, respectively.
From 1987 to 1994 he worked as a Scientific Worker, Senior Scientific Worker, Chief of the Information-Measurement Systems Dept. at the ASPA “Neftgazavtomat”. From 1994 to 1996 he was a Leading – Scientific Worker at the Institute of Cybernetics of the Academy of Sciences of Azerbaijan Republic. He was also a Professor in the Department of Electronically-Calculated System Design, Azerbaijan Technical University, where he had been teaching 1995-1996.
He joined to Department of Aeronautical Engineering, Istanbul Technical University, Turkey in 1996 as a Professor. From 2016 to 2023, he was also Head of the Aeronautical Engineering Department. He is the author about 600 scientific publications including 15 books, 34 book chapters and more than 400 international journal and international conference papers. More than 100 scientific papers are published in the Science Citation Index Expanded (SCIE) journals. His research interests include attitude determination and control, fault diagnosis, fault tolerant control, Kalman filtering and integrated navigation systems.
- Navigation
- Fault diagnosis
- Fault tolerant control
- Kalman filtering
- Satellite attitude determination and control
Oleksandr Zaporozhets
Łukasiewicz Research Network – Institute of Aviation, Warsaw, Poland
Presentation Title: Global and Local Environmental Priorities for New Aircraft Designs
Global and Local Environmental Priorities for New Aircraft Designs
EU EFACA (Environmentally Friendly Aviation for all Classes of Aircraft) project considers conceptual designing of two new types of aircraft – 80-seat regional jet with hydrogen-powered hybrid electric propulsion system (HEP) and 150-seat short-medium range jet with liquid hydrogen (LH2) fueling of the engines. For both types the Top-Level Aircraft Requirements (TLAR) are defined so as their conceptual aircraft layout, main dimensions and flight masses, schemes of power supply during the flight. Analysis of these baseline aircraft proved the reference aircraft for both of them: ATR72-600 for the HEP aircraft and Airbus-320neo for the LH2-fueled aircraft. The principles of aircraft fuel burn, emission, noise (with further impact assessment on environment) analysis and assessment of the baseline aircraft in comparison with reference aircraft in the EFACA project are formulated for three levels of their evaluation – aircraft, airport and fleet scenarios of current and future air traffic in the European perspective. For these purposes the VALDES Space was designed and developed further with detailed analysis of the aircraft design and flight performances influence on environmental impact assessment.
Between the 1978-2022 was employed in National Aviation University, Kyiv, Ukraine on the positions of Researcher, Leading Researcher, Professor, Head of the Chair, Director of the Institute, Vice Rector. From the April 2022 is employed in the Łukasiewicz Research Network – Institute of Aviation in Warsaw, Poland, on a position of the Area Research Leader – Professor. Degree of the Dr.Sc. was obtained in 1998 by the defending the thesis “Development of Models and Methods of Information Provision for Environment Protection from Civil Aviation Impact”. The title of Professor was obtained in 2004 by decision of the Academic Council of the National Aviation University. ICAO CAEP (Committee on Aviation Environmental Protection) member between 2010-2020 by nomination from Ukrainian CAA, currently a member of the MDG, WG2 and ISG groups of the CAEP. ECAC AIRMOD (Aircraft Noise Modelling Task Group) and EAEG (European Aviation and Environment Group) member from 2010. SARES member from 2015 and a member of the management board from 2023
- Aircraft
- HEP – Hybrid Electric Propulsion System
- LH2 – Liquid Hydrogen Fueling of the Engines
- Fuel burn
- Emissions
- Noise