Proceedings of the International Conference on Aerospace System Science and Engineering 2025
Springer Verlag, Singapore
978-981-95-6365-4 (ISBN)
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This book presents high-quality research in aerospace system science and engineering, covering topics such as AI for aerospace, trans-space vehicle design and integration, air and space vehicle systems, near-space vehicles, opto-electronic systems, robotics and unmanned systems, communication, navigation and surveillance, dynamics and control, intelligent sensing and information fusion, aerodynamics and aircraft design, propulsion, avionics, air traffic management, earth observation, deep space exploration, bionic micro-air/spacecraft, flight testing, and aerospace industry development.
Prof. Zhongliang Jing received his B.S., M.S., and Ph.D. degrees in Electronics and Information Technology from Northwestern Polytechnical University, Xi’an, China, in 1983, 1988, and 1994, respectively. He worked at China Leihua Electronics Technology Institute (1983–1985) and Northwestern Polytechnical University (1988–2000). Since 2000, he has been with Shanghai Jiao Tong University (SJTU), serving as Associate Dean of Electronic Information and Electrical Engineering (2001–2004) and Executive Dean of Aeronautics and Astronautics (2005–2018). He currently directs the Engineering Research Center and the Shanghai Collegiate Key Laboratory of Aerospace Science and Technology. He was Visiting Scholar at UC Berkeley (1997–1998) and Visiting Professor at Southern Illinois University (1999). His research interests include adaptive filtering, target tracking, information fusion, avionics integration, and soft robot control. Prof. Jing has published over 200 journal papers and seven monographs. He is Editor-in-Chief of aerospace systems and serves on several editorial boards. Dr. Wu Xu received his B.S. in engineering mechanics from Harbin Engineering University in 2007 and Ph.D. in solid mechanics from SJTU in 2012. He completed postdoctoral research at the University of Michigan, Ann Arbor (2012–2015), and joined SJTU’s School of Aeronautics and Astronautics in 2016, where he became Associate Professor and Vice Dean in 2022. His research focuses on solid and fracture mechanics, composite materials, and their applications in aircraft structural design. His work is supported by the National Natural Science Foundation of China, AVIC, COMAC, and the Shanghai Sailing Program. Dr. Xu has published over 70 journal papers and two books and serves as Associate Editor of Aerospace Systems. Dr. Haichao Hong received his B.S. and Ph.D. degrees from Beijing Institute of Technology in 2013 and 2019. He is now Associate Professor at SJTU’s School of Aeronautics and Astronautics. He conducted research as Visiting Ph.D. Student and Postdoctoral Fellow at the Institute of Flight System Dynamics, Technical University of Munich (TUM). His research interests include trajectory optimization, guidance and control, and flight mechanics. Dr. Hong is Senior Member of AIAA and Member of its Guidance, Navigation, and Control Technical Committee and serves as Associate Editor of the IEEE Transactions on Aerospace and Electronic Systems and on the editorial board of aerospace systems. Dr. Sutthiphong Srigrarom (Dr. Spot) received his Ph.D. from the University of Washington, USA, in 2002. He is Teaching Fellow in mechanical engineering and Senior Research Scientist at Temasek Laboratories, National University of Singapore (NUS). He previously worked at Boeing, Nanyang Technological University, and the Singapore Institute of Technology–University of Glasgow Singapore. His research covers small unmanned aircraft design, applied aerodynamics, aerial robotics, UAS applications, AI for UAS, and vision-based navigation. He teaches Small Aircraft and UAS and Swarm Robotics at NUS and is Visiting Associate Professor at TUM’s Institute of Flight System Dynamics. Since 2020, he has published over 10 journal and 40 conference papers (H-index 15, 700+ citations). Dr.-Ing. Andreas Hermanutz is Faculty Head of aerospace engineering at the Technical University of Munich (TUM) Asia campus, leading the M.Sc. program and strengthening TUM’s research network in Asia. He holds B.Sc., M.Sc., and Ph.D. degrees from TUM and has served as Research Associate at the TUM Institute of Lightweight Structures (2014–2018) and Chair of Aircraft Design (2018–2020). His research focuses on aircraft structural design, loads, and aeroelasticity, emphasizing modern simulation methods in fluid–structure interaction and the dynamics of highly flexible wings.
Hold-In, Pull-In, And Lock-In Ranges For Gnss Pll With Arctangential Detector.- Optimization Method Of The Stiffened Plates With Multi-Level Load-Transfer Structures.- Fault Diagnosis Under Variable Working Conditions En-Hanced By Diffusion Models.- Evolution Of The Instability Characteristics Of Wing-Tip Vortex Under The Effect Of Synthetic Jet.- The Effects Of Air Temperature On The Supersonic Combustion Of N-Heptane Dilute Sprays In A Model Combustor.- Investigation On The Aerodynamic Performance Characteristics Of Coaxial Contra-Rotating Propellers Under The Influence Of Blade Pitch Angles.- Civil Aircraft Aircraft Pilot Coupling Vibration Analysis And Practice.- Multi-Scale Feature Coupled Attention Mechanism For Space Object Detection Under Varying Exposure Conditions.- Design Of Power Supply Active Load Allocation Algorithm Based On Aircraft Grid Perception.- Space Faint Target Extraction And Detection Via Background Noise Modelling With Gmm.- Research On The Architecture Of Distributed Combat Simulation Platform.- Square Cupola Apriltag: A High-Precision Fiducial Marker For Pose Estimation Based On Accuracy Experiments Of Apriltag.- Matrix Stl: Concise Temporal Logic Rule For Complex Task Allocation.- Multi-Dimensional Evaluation Of Chemical Kinetic Mechanisms For Ammonia And Ammonia/Hydrogen Combustion.- Mlmskt: Mutual Learning And Multi Scale Knowledge Transfer For Aviation Bearing Fault Diagnosis Under Cross-Domain Few-Shot Learning Scenario.- Washout Algorithm Design For Evtol Aircraft Based On The Model Predictive Control Method.- Proportional Multiple-Integral Observer Based Robust Fault-Tolerant Control For Distributed Electric Propulsion Aircraft.- Identifying The Radiating Core And Predicting The Tonal Noise Radiation Of An Axial Compressor.- Hyperspectral And Multispectral Image Fusion Via Non-Local And Global Low Rank Regularization.- Conditional Variational Autoencoder For Remaining Useful Life Prediction With Spatial-Temporal Feature Fusion.- Design Of A Mission Data Handling Algorithm For A Unified Trajectory Module Based On Stanag 4586 And Mavlink.- Smooth Dubins Path Planning Based On Convolution Parameterization.- Design Optimization Of Aircraft Hybrid Electric Propulsion System Based On Full-Flight Energy Consumption Calculation.- Quantification Of Map Matching Credibility Based On Gnss Positioning Covariance.- Neural Network-Based Online Performance Degradation Prediction Of Diesel Engine Turbocharging System.- Research On Scenario Modeling Of Civil Aircrafts Based On Dodaf.- Application Method Of Dead-Zone Saturation Operation In Nonlinear Control System.- Fault Estimation For Aero-Engine Actuator Using Unknown Input Observers.- Requirements-Based Performance Optimisation Tool For Hybrid Electric Aircraft.- Research Progress On Supercritical Co2 Brayton Cycle System And Compressor For Thermal Protection Of Hypersonic Aircraft.- Visual Detection And Tracking Of Quadruped Robot From Quadrotor Using Yolov8 With Sahi And Ibvs.- Development Of A Satellite Onboard Computer Simulation Platform And Complex Network Generation Based On Renode.- Aerial Herding Of Flocks Of Birds And Interception Of Multiple Drone Targets By Distributed Chasers Using Stringnet And Heuristic Task Allocations.- Atc-Qa: A Benchmark For Evaluating Llms On Aviation Safety Compliance.- Numerical Investigation Of Flow And Heat Transfer In Turbine Disk Cavity Under Hydrogen-Oxygen Cycle Conditions.- A Methodology For Electrically Propelled Fixed-Wing Aircraft Design Based On The Integration Of Design To Cost And Rflp.- Aircraft 3d Positioning Method Based On Computer Vision.- Numerical Investigation Of Aerodynamic Interference Effects For Wing-Integrated Ducted Fans Using The Momentum Source Method.
| Erscheint lt. Verlag | 24.4.2026 |
|---|---|
| Reihe/Serie | Lecture Notes in Electrical Engineering |
| Zusatzinfo | 100 Illustrations, black and white |
| Verlagsort | Singapore |
| Sprache | englisch |
| Maße | 155 x 235 mm |
| Themenwelt | Technik ► Fahrzeugbau / Schiffbau |
| Technik ► Luft- / Raumfahrttechnik | |
| Schlagworte | Aerospace Propulsion • AI for Aerospace • Air Traffic Management • Deep space exploration • Dynamics and Control • Information Fusion • intelligent sensing |
| ISBN-10 | 981-95-6365-8 / 9819563658 |
| ISBN-13 | 978-981-95-6365-4 / 9789819563654 |
| Zustand | Neuware |
| Informationen gemäß Produktsicherheitsverordnung (GPSR) | |
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