Secure CheckoutPersonal information is secured with SSL technology.
Free ShippingFree global shipping
No minimum order.
Modern Flexible Multi-Body Dynamics Modeling Methodology for Flapping Wing Vehicles presents research on the implementation of a flexible multi-body dynamic representation of a flapping wing ornithopter that considers aero-elasticity. This effort brings advances in the understanding of flapping wing flight physics and dynamics that ultimately leads to an improvement in the performance of such flight vehicles, thus reaching their high performance potential. In using this model, it is necessary to reduce body accelerations and forces of an ornithopter vehicle, as well as to improve the aerodynamic performance and enhance flight kinematics and forces which are the design optimization objectives.
This book is a useful reference for postgraduates in mechanical engineering and related areas, as well as researchers in the field of multibody dynamics.
- Uses Lagrange equations of motion in terms of a generalized coordinate vector of the rigid and flexible bodies in order to model the flexible multi-body system
- Provides flight verification data and flight physics of highly flexible ornithoptic vehicles
- Includes an online companion site with files/codes used in application examples
Graduates and researchers with an interest in body dynamics, aerodynamics, UAVs, and vibrations
1. Bio-inspired Flight Robotics Systems
2. Flexible Multi- Body Dynamics Modeling Methodologies for Flapping Wing Vehicles
3. Bio- Inspired Flapping- wing Test platform used to implement Modern Modeling Methodology
4. Flexible Multi-Body Dynamics Modeling Methodology Implementation Avian Scale Flapping Wing Flyer
5. Aerodynamics Modeling for Flexible Multi-Body Dynamics Modeling Methodology Implementation Avian Scale Flapping Wing Flyer
6. Results Modeling Methodology Implementation and Flight Simulation
7. Concluding Remarks about Modern Modeling Methodology Implementation and Flight Physics of Avian -scale Flight Robotics Systems
- No. of pages:
- © Academic Press 2017
- 15th September 2017
- Academic Press
- Paperback ISBN:
- eBook ISBN:
Dr. Cornelia Altenbuchner is currently a Robotics Technologist at the NASA Jet Propulsion Laboratory (JPL) in Pasadena California. Cornelia earned her PhD from the University of Maryland College Park in Aerospace Engineering, during which time she conducted research at the NASA Langley Research Center and the National Institute of Aerospace. She is originally from Austria and her primary contributions are technology development in the areas of flexible multi-body dynamics modeling and simulation, robotic systems, conceptual mission design, as well as dynamics and controls. Prior to joining the NASA Jet Propulsion Laboratory in July 2016 she worked at the NASA Langley Research Center, where her primary projects involved lightweight Robotic Arms and associated systems, parts of which won the NASA Tech Briefs Invention of the year in 2015. Her work there also included the Asteroid Redirect Mission (ARM), Modular Robotic In-Space Assembly and Bio-inspired autonomous flapping wing UAV’s. Her research has been featured by National Geographic and the British Broadcasting Company (BBC). At NASA JPL, she works on robotic systems, which includes dynamic, autonomy and conceptual aspects required to support missions to Europa and Mars 2020. She is a member of the American Institute of Aeronautics and Astronautics (AIAA) Space Robotics and Automation Technical Committee and is an education and outreach enthusiast.
NASA Jet Propulsion Laboratory, Pasadena, CA, USA
Dr. James E. Hubbard, Jr. is currently the Glenn L. Martin Institute Professor at the University of Maryland and resident in Hampton, Virginia. He has an engineering career that is distinguished by more than four decades of scholarship and innovation. He began his career in 1971 as an engineering officer in the U.S. Merchant Marine serving in Vietnam. At the age of 19 qualified for and received an Unlimited Horsepower, steam, and diesel engine Marine Engineering operator’s license from the U.S. Coast Guard and was one the youngest to get such an honor. He was also one of only a handful of African American Marine Engineers in the entire U.S. Merchant fleet. He also holds a B.S., M.S. and Phd. from the at the Massachusetts Institute of Technology and during his time there he distinguished himself by receiving the Goodwin Medal for “Conspicuously Effective Teaching” and The Steward Award for Outstanding Community Service. His scholarship was also recognized as a Scott Foundation Fellow and a Vertical Flight Foundation Fellow. His work in the area of Adaptive Structures has received more than 2500 citations representing an average 100 citations a year for 25 years. He is internationally known and respected as a founding father of the field of Adaptive Structures and his original experiments in this area have become icons of the field and can be found in laboratories, classrooms and corporations around the globe. He has cofounded 3 companies and holds more than 2 dozen patents in the field of Adaptive Structures. He has received the “Key to the City” of his hometown of Danville, Virginia for lifetime achievement. He has also received the Lifetime Achievement Award of the SPIE. He has written several books in the field and more authored than 200 technical publications in his chosen field. He has also been recognized by his African American peers as the 2002 receipt of the Black Engineer of the Year “President’s Award”. His professional affiliations include, Senior Lifetime Member and Fellow of the AIAA, Fellow of the American Society of Mechanical Engineers, and Senior Member of the SPIE. Member of the National Academy of Engineering and the Virginia Academy of Science, Engineering, and Medicine.
Glenn L. Martin Institute, University of Maryland, Hampton, VA, USA
"This book presents rigorous techniques for modelling the multi-body dynamics problem in a flapping-wing vehicle as well as flexibility in the surfaces. A modern energy-based Lagrangian approach is used to derive the equations of motion. The formulation is suitable for extensions into the areas of stability analysis and control design." --The Aeronautical Journal
"This is a useful test for academics, students and hobbyists interested in studying and building flapping-wing vehicles. Though the aerodynamic models employed here are quite basic, the dynamical model is general enough that more complex aerodynamic models can easily be substituted. This could pave the way to a better understanding of the flow physics and active/passive flow control mechanisms in biological flight." --The Aeronautical Journal
Elsevier.com visitor survey
We are always looking for ways to improve customer experience on Elsevier.com.
We would like to ask you for a moment of your time to fill in a short questionnaire, at the end of your visit.
If you decide to participate, a new browser tab will open so you can complete the survey after you have completed your visit to this website.
Thanks in advance for your time.