Tuesday, 03. May 2022 | |||
Track 1 | Track 2 | Track 3 | |
09:00 - 09:30 | Opening and Welcome: President of TU Berlin, Prof. Dr. Geraldine Rauch (Room 1) |
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09:30 - 10:15 | Keynote Speech 1: Formation Flight, Dr. Stéphane Delannoy, Airbus - Chair: F. Silvestre, TU Berlin |
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10:15 - 10:45 | Coffee Break |
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10:45 - 12:15 | 1.1 A1: Adaptive Control I | 2.1 B1: Stall Protection and Disturbance Rejection | 3.1 C1: Missiles, Projectiles, and other Vehicles Guidance I |
12:15 - 13:30 | Network Lunch |
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13:30 - 15:30 | 1.2 A2: Modeling and System Identification | 2.2 B2: Vision-Based Navigation | 3.2 C2: Descent and Landing in Aerospace |
15:30 - 16:00 | Coffee Break |
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16:00 - 17:30 | 1.3 A3: Further Topics in GNC I | 2.3 B3: Spacecraft Formation & Rendezvous | 3.3 C3: Trajectory and Maneuver Planning |
19:00 - 21:00 | Reception and Get-Together |
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Wednesday, 04. May 2022 | |||
Track 1 | Track 2 | Track 3 | |
09:00 - 10:30 | 1.4 A4: Flight Dynamics & Control | 2.4 B4: Estimation and Localization | 3.4 C4: Missiles, Projectiles, and other Vehicles Guidance II |
10:30 - 11:00 | Coffee Break |
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11:00 - 11:45 | Keynote Speech 2: Ingenuity Mars Helicopter – Guidance, Navigation, and Control, Dr. Håvard Grip, NASA JPL - Chair: M. Uijt de Haag, TU Berlin |
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11:45 - 12:30 | Keynote Speech 3: Flight Control for Safe Flight – Achievements and Perspectives, Prof. Dr. Robert Luckner, TU Berlin - Chair: C. de Visser, TU Delft |
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12:30 - 13:45 | Network Lunch |
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13:45 - 15:45 | 1.5 A5: Route and Trajectory Optimization | 2.5 B5: Estimation and Navigation | 3.5 C5: Control Methods |
15:45 - 16:15 | Coffee Break |
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16:15 - 18:15 | 1.6 A6: Pilot Guidance, HMI, and Teaching | 2.6 B6: Further Topics in GNC II | 3.6 C6: Control of Flexible Systems |
20:00 - 22:00 | Conference Dinner |
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Thursday, 05. May 2022 | |||
Track 1 | Track 2 | Track 3 | |
09:00 - 09:45 | Keynote Speech 4: Enabling Path to Safe Autonomy for Urban Air Mobility, Florian Adolf, Volocopter - Chair: N. Fezans, DLR |
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09:45 - 10:15 | Coffee Break |
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10:15 - 12:15 | 1.7 A7: Adaptive Control II | 2.7 B7: Missiles, Projectiles, and other Vehicles Guidance III | 3.7 C7: Learning Techniques in Control |
12:15 - 12:30 | Short Break |
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12:30 - 13:00 | Closing Ceremony (Room 1) |
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13:00 - 14:00 | Networking Lunch |
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14:00 - 16:00 | Meeting of the Technical Committee |
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Friday, 06. May 2022 | |||
Track 1 | Track 2 | Track 3 | |
11:00 - 14:00 | Exclusive River Boat Trip* (sponsored by the Chairs of Prof. Silvestre and Prof. Uijt de Haag) |
*The Exclusive River Boat Trip is not part of the registration fee, but has been sponsored and is free of charge for whose who attend. We have limited seats. To register, please write us an email, first come first served: eurognc2022@dglr.de
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10:45 | 11:15 | 1.1.1 |
Performance Assessment of an Extremum Seeking Controller using Continuation Methods D.H. Nguyen¹, M.H. Lowenberg¹, S.A. Neild¹; ¹University of Bristol, United Kingdom | ||||
11:15 | 11:45 | 1.1.2 |
Closed–Loop MRAC Augmented LQR with Integral Action for Quadrotor UAV under the Uncertainties D. Lee¹, K. Jang¹, S. Lee¹, L. Kim¹, H. Bang¹; ¹KAIST, South Korea Presenter: Lee Jayden Dongwoo | ||||
11:45 | 12:15 | 1.1.3 |
Longitudinal Flight Path Control using Least Squares In-Flight Identification A. Köthe, AlphaLink Engineering GmbH, Germany; F. J. Silvestre, Technische Universität Berlin, Germany |
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10:45 | 11:15 | 2.1.1 |
Gaussian Process Regression-based Disturbance Compensation Control for Urban Air Mobility D. Yoon¹, C.-H. Lee¹, M.-J. Tahk¹; ¹Korea Advanced Institute of Science and Technology, South Korea | ||||
11:15 | 11:45 | 2.1.2 |
Towards Stall Detection and Learning-Based Stall Prevention for Glider Aircraft F. Hein¹, S. Notter¹, J. Axthelm¹, W. Fichter¹; ¹University of Stuttgart, Germany |
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10:45 | 11:15 | 3.1.1 |
The Comparison of the Impact Angle Controlling Guidance Laws Against Stationary Target E.H. Ata, Turkey | ||||
11:15 | 11:45 | 3.1.2 |
PIP Selection Algorithm for Lambert Guidance Considering Engagement Geometry H.I. Park¹, Y.T. Jung¹, Y.D. Kim¹; ¹Seoul National University, South Korea |
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13:30 | 14:00 | 1.2.1 |
Decoupled Parameter Identification for a Flexible Aircraft S. Olasz-Szabó¹, T. Baár¹, T. Luspay¹; ¹Institute For Computer Science and Control, ELKH, Hungary | ||||
14:00 | 14:30 | 1.2.2 |
Asymmetric Stall Modeling of the Cessna Citation II Aircraft A. Delfosse, Dassault Aviation, France; D.M. Pool¹, C.C. de Visser¹; ¹Delft University of Technology, Netherlands | ||||
14:30 | 15:00 | 1.2.3 |
System Identification of a Nonlinear UAV Model with Distributed Aerodynamics and Flexible Structure B. Herrmann¹, J. Theis¹, F. Thielecke¹; ¹Hamburg University of Technology, Germany | ||||
15:00 | 15:30 | 1.2.4 |
Engine Thrust Model Determination from Large Operational Flight Data Base C. Deiler, DLR e.V., Germany |
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13:30 | 14:00 | 2.2.1 |
Procedural Minor Body Generator Tool for Data-Driven Optical Navigation Methods C. Buonagura, Italy; M. Pugliatti, Italy; F. Topputo, Italy | ||||
14:00 | 14:30 | 2.2.2 |
Spectral Loss for Monocular Self-Supervised Depth and Visual Odometry in Rover Navigation J.I. Bravo Perez-Villar, Deimos Space, Spain; A. García-Martín¹, J. Bescós¹; ¹Autonomous University of Madrid, Spain | ||||
14:30 | 15:00 | 2.2.3 |
Visual Odometry Fusion with GNSS/IMU Localization of UAVs in Urban Areas and Integrity Monitoring M. Martens, TU Berlin, Germany |
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13:30 | 14:00 | 3.2.1 |
Output-Feedback Tube Model Predictive Control for Robust Autonomous Descent and Landing on Asteroids T. Frekhaug¹, M. Sanjurjo-Rivo¹, M. Soler¹; ¹Universidad Carlos III, Spain | ||||
14:00 | 14:30 | 3.2.2 |
Nonlinear Model Predictive Path Planning with Obstacle Avoidance for an Automated Landing Approach of Fixed-Wing Aircraft A. Steinleitner¹, Y. Bensaad, Mercedes-Benz AG, Germany; W. Fichter¹; ¹Universität Stuttgart, Germany | ||||
14:30 | 15:00 | 3.2.3 |
Definition of a Landing Strategy for a Model-Scale Reusable Rocket N. Bourliatoux¹, J.M. Riera¹, L.R. Lustosa¹; ¹ISAE-SUPAERO, France |
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16:00 | 16:30 | 1.3.1 |
Optimal Intruder Collision Avoidance for UAVs via Waypoint Tracking A. Perumalla¹, E. Johnson¹, P. Singla¹, A. Chakraborthy², L. Liebischer²; ¹Pennsylvania State University, United States ;²UtopiaCompression Corporation, United States | ||||
16:30 | 17:00 | 1.3.2 |
Passivity Based Cross-Track Control of a Fixed-Wing Aircraft J.-M. Fahmi¹, C. Woolsey¹; ¹Virginia Tech, United States | ||||
17:00 | 17:30 | 1.3.3 |
Quaternion based LQR for Free-Floating Robots without Gravity S. Vyas¹, B. Wehbe¹, S. Kumar¹; ¹DFKI GmbH, Germany |
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16:00 | 16:30 | 2.3.1 |
Cooperative Platooning and Servicing for Spacecraft Formation Flying using Model Predictive Control P. Pereira¹, B. Guerreiro¹, P. Lourenço, GMV, Portugal; ¹NOVA School of Science and Technology, Portugal Presenter: Bruno Guerreiro, NOVA School of Science and Technology | ||||
16:30 | 17:00 | 2.3.2 |
Reconfiguration of a Satellite Constellation in Circular Formation Orbit with Decentralized Model Predictive Control T. Pippia¹, V. Preda², S. Bennani², T. Keviczky¹; ¹Delft University of Technology, Netherlands ;²European Space Agency, Netherlands | ||||
17:00 | 17:30 | 2.3.3 |
Spacecraft Rendezvous Hovering Predictive Control around a Near-Rectilinear Halo Orbit J.C. Sanchez¹, F. Gavilan¹, R. Vazquez¹, C. Louembet, LAAS-CNRS, France; ¹Universidad de Sevilla, Spain Presenter: Julio C. Sanchez, University of Colorado Boulder |
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16:00 | 16:30 | 3.3.1 |
A Nonlinear Trigonometric Series Parameterization Approach for Smooth Trajectory Generation H. Hong¹, P. Piprek¹, Z. Lu¹, F. Holzapfel¹; ¹Technical University of Munich, Germany | ||||
16:30 | 17:00 | 3.3.2 |
Energy Optimal Flight Path Planing for Unmanned Aerial Vehicle in Urban Environments H. Rienecker¹, V. Hildebrand¹, H. Pfifer¹; ¹Technische Universität Dresden, Germany | ||||
17:00 | 17:30 | 3.3.3 |
Optimal Path Planning for Soaring Flight L. Bonin¹, D. Delahaye¹, A. Guitart¹, E. Feron, KAUST, Saudi Arabia; X. Prats, UPC, Spain; ¹ENAC, France Presenter: Lucas Bonin, ENAC |
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09:00 | 09:30 | 1.4.1 |
Flight Dynamics Modeling and Simulator Design for a New Class of Long-Range Guided Projectiles G.M. Vinco¹, S. Theodoulis¹, O. Sename, University Grenoble Alpes, CNRS, Grenoble INP, GIPSA-Lab, France; ¹French-German Research Institute of Saint-Louis, France | ||||
09:30 | 10:00 | 1.4.2 |
Nonlinear Model Following Control Design for a Hypersonic Waverider Configuration J. Autenrieb¹, N. Fezans¹; ¹German Aerospace Center - DE, Germany | ||||
10:00 | 10:30 | 1.4.3 |
The Virtual Flight Test Environment — A Web-Based Framework for Realistic Testing of Flight Control Laws A. Köthe¹, J. Hopf¹, R. Reinfeld¹, D. Cracau¹; ¹AlphaLink Engineering GmbH, Germany |
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09:00 | 09:30 | 2.4.1 |
The Vortex Position Estimator used for the Airbus fello’fly Transatlantic Crossing J. Adams¹, C. Frot¹, G. Ta¹; ¹Airbus, France | ||||
09:30 | 10:00 | 2.4.2 |
IMU-based Aircraft Ground Tracking using Strapdown Integration, Vibration deduced Speed Estimation and Particle Filtering M. Martens, TU Berlin, Germany |
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09:00 | 09:30 | 3.4.1 |
Mid-course Guidance for Dual-pulse Rocket Air-to-Air Missiles using Pseudospectral Sequential Convex Programming B. Kim¹, C.-H. Lee¹, M.-J. Tahk¹; ¹KAIST, South Korea | ||||
09:30 | 10:00 | 3.4.2 |
Impact Angle Control with Generalized-Polynomial Look-Angle Formulation S. Kang, China; R. Tekin, Turkey; L. Zhang, China | ||||
10:00 | 10:30 | 3.4.3 |
Impact Time Control with Bézier Curves S. Lee, South Korea; R. Tekin, Turkey |
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13:45 | 14:15 | 1.5.1 |
Robust Climate Optimal Aircraft Trajectory Planning Considering Uncertainty in Weather Forecast A. Simorgh¹, M. Soler¹, D. Gonzáles-Arribas¹; ¹Universidad Carlos III, Spain | ||||
14:15 | 14:45 | 1.5.2 |
Toward Onboard Trajectory Optimization for Fuel-Saving Climb of Aircraft with Automatic Flight Control D.M. Gierszewski¹, V. Fafard¹, F. Schweighofer¹, P. Piprek¹, M. Speckmaier¹, F. Holzapfel¹; ¹Technische Universität München, Germany | ||||
14:45 | 15:15 | 1.5.3 |
Energy-aware Route Planning for Drone Delivery Systems R. Liu¹, H.-S. Shin¹, M. Seo¹, A. Tsourdos¹; ¹Cranfield University, United Kingdom |
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13:45 | 14:15 | 2.5.1 |
Radar-Aided Inertial Navigation with Delayed Measurements M. Schneider¹, W. Fichter¹; ¹University of Stuttgart, Germany | ||||
14:15 | 14:45 | 2.5.2 |
Destination and Time-Series Inference of Moving Objects using Conditionally Markov Sequences S. Lee¹, H.-S. Shin¹; ¹Cranfield University, United Kingdom | ||||
14:45 | 15:15 | 2.5.3 |
A New Hybrid Model Approach coupling a Physical Model and an Artificial Neural Network through Joint Estimation F.A.R. Enkelmann¹, S.H. Krüger¹; ¹Technical University of Darmstadt, Germany |
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13:45 | 14:15 | 3.5.1 |
Eigenstructure Assignment Accounting for Eigenmode Participation of Control Inputs W. Meyer-Brügel¹, F.J. Silvestre¹; ¹Technische Universität Berlin, Germany | ||||
14:15 | 14:45 | 3.5.2 |
Local Stability Analysis for Sensor-based Inexact Feedback Linearization T. Cunis, University of Stuttgart, Germany | ||||
14:45 | 15:15 | 3.5.3 |
Continuous time adaptive Higher Harmonic Control R. Rubinacci¹, S. Meraglia¹, M. Lovera¹; ¹Politecnico di Milano, Italy | ||||
15:15 | 15:45 | 3.5.4 |
A new Step towards the Integration of Probabilistic µ in the Aerospace V&V Process C. Roos¹, J.-M. Biannic¹, H. Evain, CNES, France; ¹ONERA, France |
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16:15 | 16:45 | 1.6.1 |
VIGA - Virtual Instructor for General Aviation W. Rüther-Kindel¹, G. Csapo, Csapo Engineering, Germany; R. Vilter¹, F. Quaeck¹, N. Stuckert¹; ¹TH Wildau, Germany Presenter: Robert Vilter, Technical University of Applied Sciences Wildau | ||||
16:45 | 17:15 | 1.6.2 |
Analysis of DAA Alerting and Guidance using Reconstructed Trajectories that resulted in (N)MACs E. Theunissen, Netherlands Defence Academy, Netherlands; B.J.F.J. Schlössels, Logistiek Centrum Woensdrecht, Netherlands; A.B. van den Heuvel, Volkel Airbase, Netherlands; M. Jansen, Defensie Materieel Organisatie, Netherlands | ||||
17:15 | 17:45 | 1.6.3 |
Examination of the Dynamic Modes of a Single-Seater Fighter Jet During Aerial Refuelling L.H. Peristy¹, R.E. Perez¹; ¹Royal Military College of Canada, Canada | ||||
17:45 | 18:15 | 1.6.4 |
Quadditch: An Augmented Reality, Multiplayer, Aerial Robotics Game for Outreach, Education, and Research M. Foran¹, N. Nekoo¹, W. Foster¹, J.-M. Fahmi¹, N. Sakib¹, C. Woolsey¹; ¹Virginia Tech, United States Presenter: Mathew Foran, Virginia Tech |
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16:15 | 16:45 | 2.6.1 |
Attention-based DeepMoon for Crater Detection J. Song¹, N. Aouf¹, C. Honvault, European Space Agency, Netherlands; ¹City, university of london, United Kingdom | ||||
16:45 | 17:15 | 2.6.2 |
Implementation of a 3D laser-based mapping system using an sUAS swarm F. Franz, TU Berlin, Germany; M. Uijt de Haag, TU Berllin, Germany | ||||
17:15 | 17:45 | 2.6.3 |
Hopping Maneuver between Two Satellites: Simulations, Laboratory, and Flight Experiments on the International Space Station D. Watanabe¹, S. Kwok-Choon¹, J. Hudson¹, M. Romano¹; ¹Naval Postgraduate School, United States |
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16:15 | 16:45 | 3.6.1 |
Method to Account for Estimator-Induced Previewed Information Losses - Application to Synthesis of Lidar-Based Gust Load Alleviation Functions D. Cavaliere¹, N. Fezans¹, D. Kiehn¹; ¹DLR, Germany | ||||
16:45 | 17:15 | 3.6.2 |
A Novel Adaptive Aeroservoelastic Coupling Suppression Algorithm for the A330 SMART MRTT Flying Boom Control Laws R. Rodríguez Robles, Airbus UpNext, Spain Presenter: Rodney Rodríguez Robles | ||||
17:15 | 17:45 | 3.6.3 |
Robust Observer-Based Space Launcher Control with Time-Varying Objectives F. Biertümpfel¹, J. Theis, ATLAS ELEKTRONIK GmbH, Germany; H. Pfifer¹; ¹TU Dresden, Germany | ||||
17:45 | 18:15 | 3.6.4 |
Robust Line-of-sight Pointing Control On-Board a Stratospheric Balloon-Borne Platform E. Kassarian¹, F. Sanfedino¹, D. Alazard¹, J. Montel², C.-A. Chevrier²; ¹ISAE-Supaero, France ;²CNES, France |
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10:15 | 10:45 | 1.7.1 |
Incremental Passive Fault-Tolerant Control for Quadrotors With up to Three Successive Rotor Failures Y. Beyer¹, F. Gücker¹, E. Bremers¹, M. Steen¹, P. Hecker¹; ¹TU Braunschweig, Institute of Flight Guidance, Germany | ||||
10:45 | 11:15 | 1.7.2 |
Optimal Variable Wing Camber Control using Incremental Nonlinear Dynamic Inversion T.S.C. Pollack¹, E. van Kampen¹; ¹Faculty of Aerospace Engineering, Delft University of Technology, Netherlands | ||||
11:15 | 11:45 | 1.7.3 |
Accurate Tracking of Highly Dynamic Airplane Trajectories using Incremental Nonlinear Dynamic Inversion F. Gücker¹, Y. Beyer¹, M. Steen¹, P. Hecker¹; ¹Technische Universität Braunschweig, Germany |
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10:15 | 10:45 | 2.7.1 |
Guidance of Gliding Vehicles with Energy Management based on Approximate Prediction of Speed N. Cho¹, Y. Kim², H.-S. Shin¹, Y. Kim²; ¹Cranfield University, United Kingdom ;²Seoul National University, South Korea | ||||
10:45 | 11:15 | 2.7.2 |
Data-Efficient Capture Region Estimation for Tactical Missile using Active Sampling Based Gaussian Process Classification Y. Lee, South Korea; S. Lee, South Korea; Y. Kim, South Korea | ||||
11:15 | 11:45 | 2.7.3 |
Terminal Phase Nonlinear Attitude Autopilot Design for Dual-Spin Guided Projectiles S. Pineau, French-German Research Institute of Saint-Louis & CRAN, France; S. Theodoulis, French-German Research Institute of Saint-Louis, France; M. Zasadzinski¹, M. Boutayeb¹; ¹CRAN-UMR-CNRS-7039, France |
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10:15 | 10:45 | 3.7.1 |
Intelligent Aircraft Stabilization Control with Event-Triggered Scheme B. Sun, Netherlands; C. Liu, Netherlands; K. Dally, Japan; E.-J. van Kampen, Netherlands | ||||
10:45 | 11:15 | 3.7.2 |
Counter Optimization-Based Testing of Flight Envelope Protections in a Fly-By-Wire Control Law Using Deep Q-Learning D. Braun¹, R. Steffensen¹, A. Steinert¹, F. Holzapfel¹; ¹Technical University of Munich, Germany | ||||
11:15 | 11:45 | 3.7.3 |
Integrated Updraft Localization and Exploitation: End-to-End Type Reinforcement Learning Approach S. Notter¹, G. Müller¹, W. Fichter¹; ¹University of Stuttgart, Germany | ||||
11:45 | 12:15 | 3.7.4 |
Autonomous Solar-Powered Docking Station for the Unmanned Quadrotors R. Glebocki¹, A. Kopyt¹, M. Jacewicz¹, D. Florczak¹; ¹Warsaw University of Technology, Poland |