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201. 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS), JULY 2019 Paper number 359 - Computational Analysis of Urban Air Mobility Vehicles
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DOI: 10.13009/EUCASS2019-359 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS), JULY 2019 Paper number 359 Computational Analysis of Urban Air Mobility Vehicles Patricia Ventura ...
202. Numerical Investigation of a Resonance Ignition System - Christian BAUER, Paul LUNGU and Oskar J. HAIDN Institute for Turbomachinery and Flight Propulsion, Rocket Propulsion Group Technical University ...
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DOI: 10.13009/EUCASS2019-360 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Numerical Investigation of a Resonance Ignition System Christian BAUER, Paul LUNGU and Oskar J. HAIDN Institute ...
203. Numerical Solution of Supersonic Gas-Solid TwoPhase Flow - Xiang Zhaoa,b, Zhixun Xiaa, Likun Maa, Dan Michaelsb, Benveniste Natanb, Chaolong Lia
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DOI: 10.13009/EUCASS2019-362 Numerical Solution of Supersonic Gas-Solid TwoPhase Flow Xiang Zhaoa,b, Zhixun Xiaa, Likun Maa, Dan Michaelsb, Benveniste Natanb, Chaolong Lia a Department of Aerospace Science ...
204. Collision avoidance multi-vehicle distributed cooperative guidance strategy with high performance communication - Xi Zhang, Shui Yongtao, Wang Yonghai, Wang Liyan, Zhang Xuejiao Beijing Institute of Space ...
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DOI: 10.13009/EUCASS2019-366 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Collision avoidance multi-vehicle distributed cooperative guidance strategy with high performance communication Xi ...
205. The effect of single defect of RDX crystal on shock sensitivity of RDX/Al mixtures by ReaxFF-MD simulations - Ning Wang1,2, Jun Li1,2, Lu Wang3, Liguo Cheng1,2, Jing Su1,2, Xu Xiao2 and Jiefan Zhang2 1.Science ...
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DOI: 10.13009/EUCASS2019-368 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) The effect of single defect of RDX crystal on shock sensitivity of RDX/Al mixtures by ReaxFF-MD simulations Ning ...
206. The Epsilon Guidance and Control System Contributing to the High Accuracy Injection into the Orbit of the Flights - Daiki Tomita*, Hitomi Izumi*, Kensaku Tanaka*, Yuichi Noguchi*, Kazuhiro Yagi*, and Takayuki ...
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DOI: 10.13009/EUCASS2019-370 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) The Epsilon Guidance and Control System Contributing to the High Accuracy Injection into the Orbit of the ...
207. Nonlinear random response analyses of composite panels under combined supersonic aerodynamic, thermal, and acoustic loads - Hong-Beom Lee1, Yeong-Nam Kim2, Jae-Sang Park3, and In-Gul Kim4 Chungnam National ...
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DOI: 10.13009/EUCASS2019-371 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Nonlinear random response analyses of composite panels under combined supersonic aerodynamic, thermal, ...
208. The confirmation of thermal boundary parameters of the Gas Oxygen Kerosene Rich Fueled rocket engine wall - Zhixin Zhao *, Xianggeng Wei **, Lingyu Li, Xianggang Bian, Youxing Zuo (Science and Technology ...
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DOI: 10.13009/EUCASS2019-373 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) The confirmation of thermal boundary parameters of the Gas Oxygen Kerosene Rich Fueled rocket engine wall Zhixin ...
209. Investigating the Aerodynamic Interference of Control Surfaces by Artificial Neural Networks - Fazil Selcuk Gomec* Dr. Sukru Akif ERTURK** Osman AYCI** *Aerodynamics Department, Turkish Aerospace Ankara ...
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DOI: 10.13009/EUCASS2019-379 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Investigating the Aerodynamic Interference of Control Surfaces by Artificial Neural Networks Fazil Selcuk ...
210. Experimental and Computational Analysis of Single Crystal Piezoelectrical Driven Synthetic Jet Actuator - Baris Gungordu, Mark Jabbal and Atanas Popov Faculty of Engineering, University of Nottingham NG7 ...
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DOI: 10.13009/EUCASS2019-380 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Experimental and Computational Analysis of Single Crystal Piezoelectrical Driven Synthetic Jet Actuator Baris ...
211. Assessment of 4D-trajectories predictability and reliability - ?lvaro Rodr?guez-Sanz a, 1, Cecilia Claramunt Puchol a, 2, Fernando G?mez Comendador a, 3, Javier P?rez-Cast?n a, 4 , Rosa Arnaldo Vald?s ...
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DOI: 10.13009/EUCASS2019-381 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Assessment of 4D-trajectories predictability and reliability ?lvaro Rodr?guez-Sanz a, 1, Cecilia Claramunt ...
212. Implementation of CCSDS Hyperspectral Image Compression Algorithm on FPGA on board a nanosatellite - Neelanchal Joshi ? and Parth Kalgaonkar ? Team Anant, BITS Pilani Address neelanchaljoshi@gmail.com ...
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DOI: 10.13009/EUCASS2019-382 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: ADD DOINUMBER HERE Implementation of CCSDS Hyperspectral Image Compression Algorithm on FPGA ...
213. Influence of the plate leading-edge shape and thickness on the boundary layer laminar-turbulent transition at Mach number M=5 - Sergey V. Aleksandrov1, Eugenia A. Aleksandrova2, Volf Ya. Borovoy3, Vladimir ...
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DOI: 10.13009/EUCASS2019-384 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Influence of the plate leading-edge shape and thickness on the boundary layer laminar-turbulent transition ...
214. Focused research on RLV-technologies: the DLR project AKIRA - M. Sippel, S. Stappert, J. Wilken, N. Darkow DLR Institute for Space Systems, Bremen, Germany S. Cain, S. Krause DLR Institut f?r Flugsystemtechnik, ...
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DOI: 10.13009/EUCASS2019-385 8 TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) 2019 Focused research on RLV-technologies: the DLR project AKIRA M. Sippel, S. Stappert, J. Wilken, N. ...
215. Experimental comparison of attitude controllers for nanosatellites - Bello, ?lvaroa; Olfe, Karlb; Ezquerro, Jos? Miguelc; Rodr?guez, Jacobod and Lapuerta, Victoriae
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DOI: 10.13009/EUCASS2019-386 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Experimental comparison of attitude controllers for nanosatellites Bello, ?lvaroa; Olfe, Karlb; Ezquerro, ...
216. Chance-Constrained Optimal Altitude Control of a Rocket - Thomas Lew, Fabian Lyck and GianAndrea M?ller Department of Mechanical and Process Engineering, ETH Z?rich, Switzerland @student.ethz.ch
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DOI: 10.13009/EUCASS2019-388 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: ADD DOINUMBER HERE Chance-Constrained Optimal Altitude Control of a Rocket Thomas Lew, Fabian ...
217. Quasi-Static and Dynamic Response of a 1U Nano-Satellite during Launching - Ali Alhammadi*, Muneera Al-Shaibah**, Abdulla Almesmari, Thu Vu, Alexandros Tsoupos, Firas Jarrar and Prashanth Marpu, Khalifa ...
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DOI: 10.13009/EUCASS2019-398 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Quasi-Static and Dynamic Response of a 1U Nano-Satellite during Launching Ali Alhammadi*, Muneera Al-Shaibah**, ...
218. The Research of the Application of Spatial Interpolation Methods in the Two-Body Proximity Test Data of TSTO - Feng XIE*, Guanxin HONG** * School of Aeronautic Science and Engineering, Beihang University, ...
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DOI: 10.13009/EUCASS2019-400 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) The Research of the Application of Spatial Interpolation Methods in the Two-Body Proximity Test Data of ...
219. Design of Experiment Method in Objective Space for Machine Learning of Flow Structures - Runze LI*, Yufei ZHANG** and Haixin CHEN*** * School of Aerospace Engineering, Tsinghua University, Beijing, China ...
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DOI: 10.13009/EUCASS2019-403 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Design of Experiment Method in Objective Space for Machine Learning of Flow Structures Runze LI*, Yufei ...
220. Fast Homotopy Method for Binary Asteroid Landing Trajectory Optimization - Hongwei Yang * and Shuang Li ** * College of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ...
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DOI: 10.13009/EUCASS2019-404 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Fast Homotopy Method for Binary Asteroid Landing Trajectory Optimization Hongwei Yang * and Shuang Li ** ...

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