Abstract
In this study, differential flatness principle is applied in real time optimal flight trajectory generation. This principle allows formulating the desired output trajectory through Bspline parameterization. Integrating these methodologies with sequential quadratic programming, an optimal feasible trajectory that meets all the given and dynamical limits, is generated. Through this fashion, it is guaranteed to generate dynamically feasible trajectories passing, as closely as possible, by given waypoints which guide the vehicle to track its intent. For the simulation purpose, this methodology is applied to two under-actuated vehicle models (quadrotors and Dubins' airplanes)and their maneuverability for a given mission is compared to show the validity of the integrated methodologies. While the majority of similar methodologies focus on an uninformed search for a dynamically feasible trajectory through an outer checking loop, the methodology provided in this paper benefits from a guided search for a feasible solution that an optimization algorithm provides. The advantage of this study over the ones that do benefit from an optimization algorithm is that the constraints on key dynamical states of the vehicles are strictly considered in a continuous manner instead of sampling hypersurfaces. To do so, the geometrical feature of the B-splines is utilized and the constraints are checked at times in which the dynamical state of interest reaches to an extremum. This way, the constraints do not necessarily have to be linear or representable with polynomials. In this work, it is shown that these critical times are roots of polynomials with unique sets of coefficients. Moreover, the local property of B-splines is utilized for instantaneous regeneration of the trajectory without distorting the entire path and the continuity when the vehicle needs a rapid update in trajectory plan or collision avoidance. Through the knot insertion algorithm, it is shown that it is always possible to design a new trajectory that deviates from the old one before the vehicle reaches the deviation point.
Original language | English |
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Title of host publication | 2019 IEEE Aerospace Conference, AERO 2019 |
Publisher | IEEE Computer Society |
ISBN (Electronic) | 9781538668542 |
DOIs | |
Publication status | Published - Mar 2019 |
Event | 2019 IEEE Aerospace Conference, AERO 2019 - Big Sky, United States Duration: 2 Mar 2019 → 9 Mar 2019 |
Publication series
Name | IEEE Aerospace Conference Proceedings |
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Volume | 2019-March |
ISSN (Print) | 1095-323X |
Conference
Conference | 2019 IEEE Aerospace Conference, AERO 2019 |
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Country/Territory | United States |
City | Big Sky |
Period | 2/03/19 → 9/03/19 |
Bibliographical note
Publisher Copyright:© 2019 IEEE.
Funding
Emre Koyuncu is an Assistant Pro- fessor at Istanbul Technical University, Department of Aeronautical Engineer-ing. He has received his Ph.D. degree in Aerospace Engineering from Istan-bul Technical University in 2015. He was a visiting researcher at Boeing Re-search and Technology of Europe dur-ing 2013-2014, and Massachusetts In-stitute of Technology (MIT), Aero-Astro Department during 2014-2015. In his Ph.D. research, he has received SESAR WP-E HALA! Research Network Ph.D. fellowship. His research interests lie in the broad areas of aeronautics, robotics, guidance, navigation, and control theory. The application areas of his research include agile unmanned aerial vehicles, flight trajectory optimization and planning, airborne conflict avoidance and resolution, high-level autonomy in air traffic control systems, flight management and decision support systems. Prof. Koyuncu is the director of Controls and Avionics Research Group in ITU Aerospace Research Center (ITU ARC). He is the recipient of a Boeing Early Career Grant in 2015 and he is a technical committee member of IEEE Control Systems Society on Hybrid Systems and IFAC TC 7.4 Transportation Systems.
Funders | Funder number |
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Boeing | |
IEEE Control Systems Society on Hybrid Systems and IFAC TC 7.4 Transportation Systems |