A Study on the Control, Dynamics, and Hardware of Micro Aerial Biomimetic Flapping Wing Vehicles

A Study on the Control, Dynamics, and Hardware of Micro Aerial Biomimetic Flapping Wing Vehicles
Author: Siara Hunt
Publisher:
Total Pages: 190
Release: 2017
Genre: Aerodynamics
ISBN:

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Biological flight encapsulates 400 million years of evolutionary ingenuity and thus is the most efficient way to fly. If an engineering pursuit is not adhering to biomimetic inspiration, then it is probably not the most efficient design. An aircraft that is inspired by bird or other biological modes of flight is called an ornithopter and is the original design of the first airplanes. Flapping wings hold much engineering promise with the potential to produce lift and thrust simultaneously. In this research, modeling and simulation of a flapping wing vehicle is generated. The purpose of this research is to develop a control algorithm for a model describing flapping wing robotics. The modeling approach consists of initially considering the simplest possible model and subsequently building models of increasing complexity. This research finds that a proportional derivative feedback and feedforward controller applied to a nonlinear model is the most practical controller for a flapping system. Due to the complex aerodynamics of ornithopter flight, modeling and control are very difficult. Overall, this project aims to analyze and simulate different forms of biological flapping flight and robotic ornithopters, investigate different control methods, and also acquire understanding of the hardware of a flapping wing aerial vehicle.

Modeling, Optimal Kinematics, and Flight Control of Bio-inspired Flapping Wing Micro Air Vehicles

Modeling, Optimal Kinematics, and Flight Control of Bio-inspired Flapping Wing Micro Air Vehicles
Author: Zaeem Khan
Publisher:
Total Pages:
Release: 2009
Genre: Airplanes
ISBN: 9781109386585

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?Pub Inc Micro air vehicles (MAV) provide an attractive solution for carrying out missions such as searching for survivors inside burning buildings or under collapsed structures, remote sensing of hazardous chemical and radiation leaks and surveillance and reconnaissance. MAVs can be miniature airplanes and helicopters, however, nature has micro air vehicles in the form of insects and hummingbirds, which outperform conventional designs and are therefore, ideal for MAV missions. Hence, there is a need to develop a biomimetic flapping wing micro air vehicle (FWMAV). In this work, theoretical and experimental research is undertaken in order to reverse engineer the complicated design of biological MAVs. Mathematical models of flapping wing kinematics, aerodynamics, thorax musculoskeletal system and flight dynamics were developed and integrated to form a generic model of insect flight. For experimental work, a robotic flapper was developed to mimic insect wing kinematics and aerodynamics. Using a combination of numerical optimization, experiments and theoretical analysis, optimal wing kinematics and thorax dynamics was determined. The analysis shows remarkable features in insect wings which significantly improve aerodynamic performance. Based on this study, tiny flapping mechanisms were developed for FWMAV application. These mechanisms mimic the essential mechanics of the insect thorax. Experimental evaluation of these mechanisms confirmed theoretical findings. The analysis of flight dynamics revealed the true nature of insect flight control which led to the development of controllers for semi-autonomous flight of FWMAV. Overall, this study not only proves the feasibility of biomimetic flapping wing MAV but also proves its advantages over conventional designs. In addition, this work also motivates further research in biological systems.

The DelFly

The DelFly
Author: G.C.H.E. de Croon
Publisher: Springer
Total Pages: 221
Release: 2015-11-26
Genre: Technology & Engineering
ISBN: 9401792089

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This book introduces the topics most relevant to autonomously flying flapping wing robots: flapping-wing design, aerodynamics, and artificial intelligence. Readers can explore these topics in the context of the "Delfly", a flapping wing robot designed at Delft University in The Netherlands. How are tiny fruit flies able to lift their weight, avoid obstacles and predators, and find food or shelter? The first step in emulating this is the creation of a micro flapping wing robot that flies by itself. The challenges are considerable: the design and aerodynamics of flapping wings are still active areas of scientific research, whilst artificial intelligence is subject to extreme limitations deriving from the few sensors and minimal processing onboard. This book conveys the essential insights that lie behind success such as the DelFly Micro and the DelFly Explorer. The DelFly Micro, with its 3.07 grams and 10 cm wing span, is still the smallest flapping wing MAV in the world carrying a camera, whilst the DelFly Explorer is the world's first flapping wing MAV that is able to fly completely autonomously in unknown environments. The DelFly project started in 2005 and ever since has served as inspiration, not only to many scientific flapping wing studies, but also the design of flapping wing toys. The combination of introductions to relevant fields, practical insights and scientific experiments from the DelFly project make this book a must-read for all flapping wing enthusiasts, be they students, researchers, or engineers.

Modelling and Controlling a Bio-inspired Flapping-wing Micro Aerial Vehicle

Modelling and Controlling a Bio-inspired Flapping-wing Micro Aerial Vehicle
Author: David Everett Smith
Publisher:
Total Pages:
Release: 2012
Genre: Airplanes
ISBN:

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The objective of this research is to verify the three degree of freedom capabilities of a bio-inspired quad flapping-wing micro aerial vehicle in simulation and in hardware. The simulation employs a nonlinear plant model and input-output feedback linearization controller to verify the three degree of freedom capabilities of the vehicle. The hardware is a carbon fiber test bench with four flapping wings and an embedded avionics system which is controlled via a PD linear controller. Verification of the three degree of freedom capabilities of the quad flapping-wing concept is achieved by analyzing the response of both the simulation and test bench to pitch, roll, and yaw attitude commands.

A Closed Loop Research Platform that Enables Dynamic Control of Wing Gait Patterns in a Vertically Constrained Flapping Wing - Micro Air Vehicle

A Closed Loop Research Platform that Enables Dynamic Control of Wing Gait Patterns in a Vertically Constrained Flapping Wing - Micro Air Vehicle
Author: Hermanus Van Niekerk Botha
Publisher:
Total Pages: 58
Release: 2016
Genre: Machine learning
ISBN:

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Research in Flapping Wing - Micro Air Vehicles(FW-MAVs) has been growing in recent years. Work ranging from mechanical designs to adaptive control algorithms are being developed in pursuit of mimicking natural flight. FW-MAV technology can be applied in a variety of use cases such a military application and surveillance, studying natural ecological systems, and hobbyist commercialization. Recent work has produced small scale FW-MAVs that are capable of hovering and maneuvering. Researchers control maneuvering in various ways, some of which involve making small adjustments to the core wing motion patterns (wing gaits) which determine how the wings flap. Adaptive control algorithms can be implemented to dynamically change these wing motion patterns to allow one to use gait based modification controllers even after damage to a vehicle or its wings occur. This thesis will create and present a hardware research platform that enables hardware-in-the-loop experimentation with core wing gait adaptation methods.

Biomimetic Unmanned Aerial System

Biomimetic Unmanned Aerial System
Author: Jonathan Maglasang
Publisher:
Total Pages: 144
Release: 2016-11-22
Genre:
ISBN: 9783659964886

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Flight Dynamics and System Identification for Modern Feedback Control

Flight Dynamics and System Identification for Modern Feedback Control
Author: Jared A Grauer
Publisher: Woodhead Publishing
Total Pages: 0
Release: 2013-08-31
Genre: Technology & Engineering
ISBN: 9780857094667

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Unmanned air vehicles are becoming increasingly popular alternatives for private applications which include, but are not limited to, fire fighting, search and rescue, atmospheric data collection, and crop surveys, to name a few. Among these vehicles are avian-inspired, flapping-wing designs, which are safe to operate near humans and are required to carry payloads while achieving manoeuverability and agility in low speed flight. Conventional methods and tools fall short of achieving the desired performance metrics and requirements of such craft. Flight dynamics and system identification for modern feedback control provides an in-depth study of the difficulties associated with achieving controlled performance in flapping-wing, avian-inspired flight, and a new model paradigm is derived using analytical and experimental methods, with which a controls designer may then apply familiar tools. This title consists of eight chapters and covers flapping-wing aircraft and flight dynamics, before looking at nonlinear, multibody modelling as well as flight testing and instrumentation. Later chapters examine system identification from flight test data, feedback control and linearization.

Attitude and Position Control of Flapping-wing Micro Aerial Vehicles

Attitude and Position Control of Flapping-wing Micro Aerial Vehicles
Author: Ning Che
Publisher:
Total Pages:
Release: 2018
Genre:
ISBN:

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Compared with the fixed-wing and rotor aircraft, the flapping-wing micro aerial vehicle is of great interest to many communities because of its high efficiency and flexible maneuverability. However, issues such as the small size of the vehicles, complex dynamics and complicated systems due to uncertainty, nonlinearity, and multi-coupled parameters cause several significant challenges in construction and control. In this thesis, based on Euler angle and unit quaternion representations, the backstepping technique is used to design attitude stabilization controllers and position tracking controllers for a good control performance of a flapping-wing micro aerial vehicle. The attitude control of a apping{wing micro aerial vehicle is achieved by controlling the aerodynamic forces and torques, which are highly nonlinear and time{varying. To control such a complex system, a dynamic model is derived by using the Newton{Euler method. Based on the mathematical model, the backstepping technique is applied with the Lyapunov stability theory for the controller design. Moreover, because a flapping-wing micro aerial vehicle has very exible wings and oscillatory flight characteristics, the adaptive fuzzy control law as well as H1 control strategy are also used to estimate the unknown parameters and attenuate the impact of external disturbances. What is more, due to the problem of the gimbal lock of Euler angles, the unit quaternion representation is used afterwards. As for position control, the forward movement is controlled by the thrust and lift force generated by the wings of flapping-wing micro aerial vehicles. To make the actual position and velocity follow the desired trajectory and velocity, the backstepping scheme is used based on a unit quaternion representation. In order to reduce the complexity of differentiation of the virtual control in the design process, a dynamic surface control method is then used by the idea of a low-pass filter. Matlab simulation results prove the mathematical feasibility and also illustrate that all the proposed controllers have a stable control performance.

Immunology Memory-based Approach with Applications to Flapping Wing Micro Aerial Vehicles (MAVS)

Immunology Memory-based Approach with Applications to Flapping Wing Micro Aerial Vehicles (MAVS)
Author: Liguo Weng
Publisher:
Total Pages: 156
Release: 2010
Genre: Biomimicry
ISBN:

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Develops a dynamic model for a flapping wing micro aerial vehicle (MAV) that is based on the knowledge of skeletal and muscular components of hummingbirds. Applies the memory-based control approach to the flapping wing system as a fundamental comparison to the immunology/memory-based control approach. Applies the immunololgy/memory-based control approach to the flapping wing system to control the MAV's flapping motion.

Springs and Wings

Springs and Wings
Author: James Lynch
Publisher:
Total Pages: 0
Release: 2023
Genre:
ISBN:

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In the last decade, roboticists have had significant success building centimeter-scale flapping wing micro aerial vehicles (FWMAVs) inspired by the flight of insects. Evidence suggests that insects store and release energy in the thoracic exoskeleton to improve energy efficiency by flapping at resonance. Insect-inspired micro flying robots have also leveraged resonance to improve efficiency, but they have discovered that operating at the resonant frequency leads to issues with flight control. This research seeks to investigate the roles that elasticity, aerodynamics, and muscle dynamics play in the emergent dynamics of flapping flight by studying elastic flapping spring-wing systems using dynamically-scaled robophysical models of spring-wings. Studying the dynamics of a robot with comparable features enables the validation of models from biology that are otherwise difficult to test in living insects, the generation of new hypotheses, and the development of novel FWMAV designs. In Chapter 1, the spring-wing system is characterized as a nonlinear spring-mass-damper model. A robophysical model validates that such systems gain energetic benefits from operating at resonance, but reveals that the benefit scales with an underappreciated dimensionless ratio of inertial to aerodynamic forces, the Weis-Fogh number. We show through dimensional analysis that any real system, living or robotic, must balance the mechanical advantage gained from operating at resonance with diminishing returns in efficiency. Chapter 2 further explores the impact of the Weis-Fogh number on flapping dynamics, showing that responsiveness to control inputs is reduced and resistance to environmental perturbations is increased as the dimensionless ratio increases. Together with calculations of Weis-Fogh number in insects, these studies illustrate tradeoffs that drive evolution of resonant flight in nature and guide development of future FWMAVs with elastic energy exchange. In the second half of the thesis, muscle dynamics are introduced in the form of a simplified model of self-excited asynchronous insect muscle. In Chapter 3, a linear feedback model adapted from experiments on insect flight muscle is developed and integrated with the spring-wing model, producing a system that generates steady flapping via limit-cycle oscillations despite the absence of periodic control inputs. The model is explored analytically, in simulation, and via implementation on the robotic spring-wing. Novel dynamic characteristics that enable adaptation to damage and passive response to wing collisions are described. Chapter 4 leverages the asynchronous feedback model as part of an interdisciplinary study of the evolution of asynchronous muscle. Phylogenetic analysis, direct measurement of insect muscle dynamics, and experiments on the robophysical system show that evolutionary transitions between periodically forced and self-excited insect muscle were likely made possible by a "bridge" in the dynamic parameter space that could be traversed under specific conditions. The asynchronous spring-wing model provides new insight into the flight and evolution of some of the most agile insects in nature, and presents a novel adaptive control scheme for future FWMAVs.