
Flapping Wing Vehicles
Numerical and Experimental Approach
CRC Press
1st Edition
Published on 25. September 2023
Book
Paperback/Softback
405 pages
978-1-032-07413-9 (ISBN)
Description
Flapping wing vehicles (FWVs) have unique flight characteristics and the successful flight of such a vehicle depends upon efficient design of the flapping mechanisms while keeping the minimum weight of the structure. Flapping Wing Vehicles: Numerical and Experimental Approach discusses design and kinematic analysis of various flapping wing mechanisms, measurement of flap angle/flapping frequency, and computational fluid dynamic analysis of motion characteristics including manufacturing techniques. The book also includes wind tunnel experiments, high-speed photographic analysis of aerodynamic performance, soap film visualization of 3D down washing, studies on the effect of wing rotation, figure-of-eight motion characteristics, and more.
Features
Covers all aspects of FWVs needed to design one and understand how and why it flies
Explains related engineering practices including flapping mechanism design, kinematic analysis, materials, manufacturing, and aerodynamic performance measures using wind tunnel experiments
Includes CFD analysis of 3D wing profile, formation flight of FWVs, and soap film visualization of flapping wings
Discusses dynamics and image-based control of a group of ornithopters
Explores indigenous PCB design for achieving altitude and attitude control
This book is aimed at researchers and graduate students in mechatronics, materials, aerodynamics, robotics, biomimetics, vehicle design and MAV/UAV.
Features
Covers all aspects of FWVs needed to design one and understand how and why it flies
Explains related engineering practices including flapping mechanism design, kinematic analysis, materials, manufacturing, and aerodynamic performance measures using wind tunnel experiments
Includes CFD analysis of 3D wing profile, formation flight of FWVs, and soap film visualization of flapping wings
Discusses dynamics and image-based control of a group of ornithopters
Explores indigenous PCB design for achieving altitude and attitude control
This book is aimed at researchers and graduate students in mechatronics, materials, aerodynamics, robotics, biomimetics, vehicle design and MAV/UAV.
More details
Language
English
Place of publication
London
United Kingdom
Publishing group
Taylor & Francis Ltd
Target group
College/higher education
Illustrations
332 s/w Zeichnungen, 85 s/w Tabellen, 472 s/w Abbildungen, 140 s/w Photographien bzw. Rasterbilder
85 Tables, black and white; 332 Line drawings, black and white; 140 Halftones, black and white; 472 Illustrations, black and white
Dimensions
Height: 234 mm
Width: 156 mm
Thickness: 23 mm
Weight
644 gr
ISBN-13
978-1-032-07413-9 (9781032074139)
Copyright in bibliographic data and cover images is held by Nielsen Book Services Limited or by the publishers or by their respective licensors: all rights reserved.
Schweitzer Classification
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09/2021
1st Edition
CRC Press
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09/2021
1st Edition
CRC Press
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E-Book
09/2021
1st Edition
CRC Press
€93.49
Available for download
Persons
Prof. Lung-Jieh Yang received Ph.D. from Institute of Applied Mechanics, National Taiwan University in 1997 and has one-year sabbatical leave to Caltech for learning MEMS technology during 2000-2001. He is now a full professor and the former department chair of Mechanical Engineering, Tamkang University, and is also the editor-in-chief of "Journal of Applied Science and Engineering" (an EI/Scopus/ESCI journal with ISSN 1560-6686). Prof. Yang devoted to the researches of polymer microelectromechanical systems (polymer MEMS, especially parylene and gelatin techniques) and flapping wing micro air vehicles (FWMAVs) for 20 years and has ever published 66 journal papers, more than 100 conference papers, 2 textbooks about MEMS, and 17 US/Taiwan patents about polymer MEMS and micro ornithopters. He has ever been the Taiwan side's PI of the Indo-Taiwan project "Design, Development and Formation Control of Micro Ornithopters (102-2923-E-032-001-MY3)" during 2013-2016. In this project he built up not only the technical cooperation between India and Taiwan but also coauthors several international journal papers with some Indian scholars/institutes. Prof. Yang hosted 2 international conferences including "The International Conference on Biomimetic and Ornithopters (ICBAO-2015)" and "The International Conference on Intelligent Unmanned Systems (ICIUS-2017)." He is also one of the vice presidents of International Society of Intelligent Unmanned Systems (ISIUS) since 2017.
Dr Esakki Balasubramanian received PhD in the field of Robotics and Control at Concordia University, Montreal, Canada. He has published two books, more than 100 Journals and Conference papers and 7 patents have been applied. He received grants from various Government of India funding programmes supported through DST, DRDO, ISRO, DBT. He has collaborated with Taiwan scientists under Indo-Taiwan schema (2013-16) for the development of micro aerial flapping wing vehicles and formation control through image processing techniques. He has designed a table top test rig integrated with two load cells to measure the aerodynamic forces of flapping wing vehicles funded by DRDO - AR & DB. He has also collaborated with Canadian scientists in developing and deployment of UAVs for railway bridge inspection. He developed amphibious UAV for collection of water samples in remote water bodies under Indo-Korea research schemes funded by DST, Govt. of India. His team developed UAVs for diverse applications including power line inspection, telecom tower inspection and radiation measurement, environmental monitoring, surveillance and traffic monitoring etc. His team won the first prize of Rs 5 lakhs in a National level competition organized by Power Grid Corporation Limited and prestigious telecom sector Aegis Graham bell award in the category of best innovative business model 2014. His research interests are UAVs, robotics, control and sensors with online data acquisition systems.
Dr Esakki Balasubramanian received PhD in the field of Robotics and Control at Concordia University, Montreal, Canada. He has published two books, more than 100 Journals and Conference papers and 7 patents have been applied. He received grants from various Government of India funding programmes supported through DST, DRDO, ISRO, DBT. He has collaborated with Taiwan scientists under Indo-Taiwan schema (2013-16) for the development of micro aerial flapping wing vehicles and formation control through image processing techniques. He has designed a table top test rig integrated with two load cells to measure the aerodynamic forces of flapping wing vehicles funded by DRDO - AR & DB. He has also collaborated with Canadian scientists in developing and deployment of UAVs for railway bridge inspection. He developed amphibious UAV for collection of water samples in remote water bodies under Indo-Korea research schemes funded by DST, Govt. of India. His team developed UAVs for diverse applications including power line inspection, telecom tower inspection and radiation measurement, environmental monitoring, surveillance and traffic monitoring etc. His team won the first prize of Rs 5 lakhs in a National level competition organized by Power Grid Corporation Limited and prestigious telecom sector Aegis Graham bell award in the category of best innovative business model 2014. His research interests are UAVs, robotics, control and sensors with online data acquisition systems.
Author
Tamkang University, Tamsui, Taiwan
Vel Tech Rangarajan Dr Sagunthala R & D Institute of Science and Technology, India
Content
1. INTRODUCTION TO MICRO AERIAL VEHICLES. 2. IN-SITU LIFT MEASUREMENT USING PVDF WING SENSOR. 3. FLAPPING WING MECHANISM DESIGN. 4. FABRICATION OF FLAPPING WING MICRO AIR VEHICLES. 5. FLAPPING WING DESIGN. 6. CLAP-AND-FLING FLAPPING. 7. COMPUTATIONAL FLUID DYNAMICS ANALYSIS OF FLAPPING WINGS. 8. SOAP FILM FLOW VISUALIZATION OF FLAPPING WING MOTION. 9. DYNAMICS AND IMAGE-BASED CONTROL OF FLAPPING WING MICRO AERIAL VEHICLES. 10. ARDUINO-BASED FLIGHT CONTROL OF ORNITHOPTERS. 11. SERVO DRIVEN FLAPPING WING VEHICLES. 12. FIGURE-OF-EIGHT MOTION AND FLAPPING WING ROTATION.