Buch, Englisch, 629 Seiten, Format (B × H): 155 mm x 235 mm
Volume II
Buch, Englisch, 629 Seiten, Format (B × H): 155 mm x 235 mm
Reihe: Lecture Notes in Mechanical Engineering
ISBN: 978-981-953006-9
Verlag: Springer
This book includes original, peer-reviewed research papers from the 2nd Aerospace Frontiers Conference (AFC 2025), held in Beijing, China on Apr. 11-14, 2025. The topics covered include but are not limited to: Overall Design and Autonomous Intelligence Technology of Intelligent Unmanned Aerial Vehicles, Aerodynamics of Aerospace Vehicles, New Aerospace Propulsion Systems, Intelligent and Morphing Aircraft Technology, Recent Advances and New Challenges in Aircraft Strength Technology, Complexity Sciences in Aerospace, Intelligent Control and Trajectory Planning of Aerospace Vehicles, Frontiers in Low-Altitude Traffic, Intelligent Sensing and Processing of Aerospace Information, Space Intelligent Control Technology, Dynamics and Control of Space Unmanned Systems, Lightweight Design and Evaluation in Aerospace Equipment, making the book a valuable asset for researchers, engineers, and university students alike.
Zielgruppe
Research
Fachgebiete
- Technische Wissenschaften Technik Allgemein Konstruktionslehre und -technik
- Technische Wissenschaften Verkehrstechnik | Transportgewerbe Luft- und Raumfahrttechnik, Luftverkehr
- Technische Wissenschaften Elektronik | Nachrichtentechnik Elektronik
- Technische Wissenschaften Sonstige Technologien | Angewandte Technik Astronautik
- Technische Wissenschaften Elektronik | Nachrichtentechnik Nachrichten- und Kommunikationstechnik Regelungstechnik
Weitere Infos & Material
A method for situation awareness of unmanned aerial vehicle based on octree map.- Study on Dynamic Search Area Matching Model of Missile Early Warning Radar based on Target Guidance Information.- Intelligent Process Design Based on Structured Data Modeling for Human-Robot Collaborative Assembly.- Research on Human-Robot Collaborative Riveting for
Helicopter Assembly.- Research on the quantitative analysis method of coupling relationship of limit protection parameters of aero-engine based on SMDV.
