Upwind Dynamic Soaring of Albatrosses and Uavs ⇑ Philip L
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Soaring Weather
Chapter 16 SOARING WEATHER While horse racing may be the "Sport of Kings," of the craft depends on the weather and the skill soaring may be considered the "King of Sports." of the pilot. Forward thrust comes from gliding Soaring bears the relationship to flying that sailing downward relative to the air the same as thrust bears to power boating. Soaring has made notable is developed in a power-off glide by a conven contributions to meteorology. For example, soar tional aircraft. Therefore, to gain or maintain ing pilots have probed thunderstorms and moun altitude, the soaring pilot must rely on upward tain waves with findings that have made flying motion of the air. safer for all pilots. However, soaring is primarily To a sailplane pilot, "lift" means the rate of recreational. climb he can achieve in an up-current, while "sink" A sailplane must have auxiliary power to be denotes his rate of descent in a downdraft or in come airborne such as a winch, a ground tow, or neutral air. "Zero sink" means that upward cur a tow by a powered aircraft. Once the sailcraft is rents are just strong enough to enable him to hold airborne and the tow cable released, performance altitude but not to climb. Sailplanes are highly 171 r efficient machines; a sink rate of a mere 2 feet per second. There is no point in trying to soar until second provides an airspeed of about 40 knots, and weather conditions favor vertical speeds greater a sink rate of 6 feet per second gives an airspeed than the minimum sink rate of the aircraft. -
Hang Glider: Range Maximization the Problem Is to Compute the flight Inputs to a Hang Glider So As to Provide a Maximum Range flight
Hang Glider: Range Maximization The problem is to compute the flight inputs to a hang glider so as to provide a maximum range flight. This problem first appears in [1]. The hang glider has weight W (glider plus pilot), a lift force L acting perpendicular to its velocity vr relative to the air, and a drag force D acting in a direction opposite to vr. Denote by x the horizontal position of the glider, by vx the horizontal component of the absolute velocity, by y the vertical position, and by vy the vertical component of absolute velocity. The airmass is not static: there is a thermal just 250 meters ahead. The profile of the thermal is given by the following upward wind velocity: 2 2 − x −2.5 x u (x) = u e ( R ) 1 − − 2.5 . a m R We take R = 100 m and um = 2.5 m/s. Note, MKS units are used through- out. The upwind profile is shown in Figure 1. Letting η denote the angle between vr and the horizontal plane, we have the following equations of motion: 1 x˙ = vx, v˙x = m (−L sin η − D cos η), 1 y˙ = vy, v˙y = m (L cos η − D sin η − W ) with q vy − ua(x) 2 2 η = arctan , vr = vx + (vy − ua(x)) , vx 1 1 L = c ρSv2,D = c (c )ρSv2,W = mg. 2 L r 2 D L r The glider is controlled by the lift coefficient cL. The drag coefficient is assumed to depend on the lift coefficient as 2 cD(cL) = c0 + kcL where c0 = 0.034 and k = 0.069662. -
2.1 ANOTHER LOOK at the SIERRA WAVE PROJECT: 50 YEARS LATER Vanda Grubišic and John Lewis Desert Research Institute, Reno, Neva
2.1 ANOTHER LOOK AT THE SIERRA WAVE PROJECT: 50 YEARS LATER Vanda Grubiˇsi´c∗ and John Lewis Desert Research Institute, Reno, Nevada 1. INTRODUCTION aerodynamically-minded Germans found a way to contribute to this field—via the development ofthe In early 20th century, the sport ofmanned bal- glider or sailplane. In the pre-WWI period, glid- loon racing merged with meteorology to explore ers were biplanes whose two wings were held to- the circulation around mid-latitude weather systems gether by struts. But in the early 1920s, Wolfgang (Meisinger 1924; Lewis 1995). The information Klemperer designed and built a cantilever mono- gained was meager, but the consequences grave— plane glider that removed the outside rigging and the death oftwo aeronauts, LeRoy Meisinger and used “...the Junkers principle ofa wing with inter- James Neeley. Their balloon was struck by light- nal bracing” (von Karm´an 1967, p. 98). Theodore ening in a nighttime thunderstorm over central Illi- von Karm´an gives a vivid and lively account of nois in 1924 (Lewis and Moore 1995). After this the technical accomplishments ofthese aerodynam- event, the U.S. Weather Bureau halted studies that icists, many ofthem university students, during the involved manned balloons. The justification for the 1920s and 1930s (von Karm´an 1967). use ofthe freeballoon was its natural tendency Since gliders are non-powered craft, a consider- to move as an air parcel and thereby afford a La- able skill and familiarity with local air currents is grangian view ofthe phenomenon. Just afterthe required to fly them. In his reminiscences, Heinz turn ofmid-20th century, another meteorological ex- Lettau also makes mention ofthe influence that periment, equally dangerous, was accomplished in experiences with these motorless craft, in his case the lee ofthe Sierra Nevada. -
Alexander 2013 Principles-Of-Animal-Locomotion.Pdf
.................................................... Principles of Animal Locomotion Principles of Animal Locomotion ..................................................... R. McNeill Alexander PRINCETON UNIVERSITY PRESS PRINCETON AND OXFORD Copyright © 2003 by Princeton University Press Published by Princeton University Press, 41 William Street, Princeton, New Jersey 08540 In the United Kingdom: Princeton University Press, 3 Market Place, Woodstock, Oxfordshire OX20 1SY All Rights Reserved Second printing, and first paperback printing, 2006 Paperback ISBN-13: 978-0-691-12634-0 Paperback ISBN-10: 0-691-12634-8 The Library of Congress has cataloged the cloth edition of this book as follows Alexander, R. McNeill. Principles of animal locomotion / R. McNeill Alexander. p. cm. Includes bibliographical references (p. ). ISBN 0-691-08678-8 (alk. paper) 1. Animal locomotion. I. Title. QP301.A2963 2002 591.47′9—dc21 2002016904 British Library Cataloging-in-Publication Data is available This book has been composed in Galliard and Bulmer Printed on acid-free paper. ∞ pup.princeton.edu Printed in the United States of America 1098765432 Contents ............................................................... PREFACE ix Chapter 1. The Best Way to Travel 1 1.1. Fitness 1 1.2. Speed 2 1.3. Acceleration and Maneuverability 2 1.4. Endurance 4 1.5. Economy of Energy 7 1.6. Stability 8 1.7. Compromises 9 1.8. Constraints 9 1.9. Optimization Theory 10 1.10. Gaits 12 Chapter 2. Muscle, the Motor 15 2.1. How Muscles Exert Force 15 2.2. Shortening and Lengthening Muscle 22 2.3. Power Output of Muscles 26 2.4. Pennation Patterns and Moment Arms 28 2.5. Power Consumption 31 2.6. Some Other Types of Muscle 34 Chapter 3. -
Design and Flight-Path Simulation of a Dynamic-Soaring UAV
PhD Dissertations and Master's Theses Summer 7-2021 Design and Flight-Path Simulation of a Dynamic-Soaring UAV Gladston Joseph [email protected] Follow this and additional works at: https://commons.erau.edu/edt Part of the Aerodynamics and Fluid Mechanics Commons, Aeronautical Vehicles Commons, Navigation, Guidance, Control and Dynamics Commons, Other Aerospace Engineering Commons, and the Propulsion and Power Commons Scholarly Commons Citation Joseph, Gladston, "Design and Flight-Path Simulation of a Dynamic-Soaring UAV" (2021). PhD Dissertations and Master's Theses. 599. https://commons.erau.edu/edt/599 This Thesis - Open Access is brought to you for free and open access by Scholarly Commons. It has been accepted for inclusion in PhD Dissertations and Master's Theses by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. Design and Flight-Path Simulation of a Dynamic-Soaring UAV By Gladston Joseph A Thesis Submitted to the Faculty of Embry-Riddle Aeronautical University In Partial Fulfillment of the Requirements for the Degree of Master of Science in Aerospace Engineering July 2021 Embry-Riddle Aeronautical University Daytona Beach, Florida Daewon Kim 8/3/2021 8/3/2021 8/3/2021 iii ACKNOWLEDGEMENTS “In the beginning God created the heavens and the earth” - Genesis 1:1 NKJV I would like to thank my advisors, Dr. Vladimir Golubev, and Dr. Snorri Gudmundsson for their expertise, guidance and the moral support. I would also like to extend my acknowledgement to Dr. William Mackunis and Dr. Hever Moncayo for their guidance in the development of control laws. My gratitude goes towards my father, Mr. -
TOTAL ENERGY COMPENSATION in PRACTICE by Rudolph Brozel ILEC Gmbh Bayreuth, Germany, September 1985 Edited by Thomas Knauff, & Dave Nadler April, 2002
TOTAL ENERGY COMPENSATION IN PRACTICE by Rudolph Brozel ILEC GmbH Bayreuth, Germany, September 1985 Edited by Thomas Knauff, & Dave Nadler April, 2002 This article is copyright protected © ILEC GmbH, all rights reserved. Reproduction with the approval of ILEC GmbH only. FORWARD Rudolf Brozel and Juergen Schindler founded ILEC in 1981. Rudolf Brozel was the original designer of ILEC variometer systems and total energy probes. Sadly, Rudolph Brozel passed away in 1998. ILEC instruments and probes are the result of extensive testing over many years. More than 6,000 pilots around the world now use ILEC total energy probes. ILEC variometers are the variometer of choice of many pilots, for both competition and club use. Current ILEC variometers include the SC7 basic variometer, the SB9 backup variometer, and the SN10 flight computer. INTRODUCTION The following article is a summary of conclusions drawn from theoretical work over several years, including wind tunnel experiments and in-flight measurements. This research helps to explain the differences between the real response of a total energy variometer and what a soaring pilot would prefer, or the ideal behaviour. This article will help glider pilots better understand the response of the variometer, and also aid in improving an existing system. You will understand the semi-technical information better after you read the following article the second or third time. THE INFLUENCE OF ACCELERATION ON THE SINK RATE OF A SAILPLANE AND ON THE INDICATION OF THE VARIOMETER. Astute pilots may have noticed when they perform a normal pull-up manoeuvre, as they might to enter a thermal; the TE (total energy) variometer first indicates a down reading, whereas the non-compensated variometer would rapidly go to the positive stop. -
DYNAMIC SOARING UAV GLIDERS by Jeffrey H. Koessler
Dynamic Soaring UAV Gliders Item Type text; Electronic Dissertation Authors Koessler, Jeffrey H. Publisher The University of Arizona. Rights Copyright © is held by the author. Digital access to this material is made possible by the University Libraries, University of Arizona. Further transmission, reproduction or presentation (such as public display or performance) of protected items is prohibited except with permission of the author. Download date 07/10/2021 13:32:45 Link to Item http://hdl.handle.net/10150/627980 DYNAMIC SOARING UAV GLIDERS by Jeffrey H. Koessler __________________________ Copyright © Jeffrey H. Koessler 2018 A Dissertation Submitted to the Faculty of the DEPARTMENT OF AEROSPACE & MECHANICAL ENGINEERING In Partial Fulfillment of the Requirements For the Degree of DOCTOR OF PHILOSOPHY WITH A MAJOR IN AEROSPACE ENGINEERING In the Graduate College THE UNIVERSITY OF ARIZONA 2018 THEUNIVERSITY OF ARIZONA GRADUATE COLLEGE Date: 01 May 2018 RIZONA 2 STATEMENT BY AUTHOR This dissertation has been submitted in partial fulfillment of the requirements for an advanced degree at the University of Arizona and is deposited in the University Library to be made available to borrowers under rules of the Library. Brief quotations from this dissertation are allowable without special permission, provided that an accurate acknowledgement of the source is made. Requests for permission for extended quotation from or reproduction of this manuscript in whole or in part may be granted by the copyright holder. SIGNED: Jeffrey H. Koessler 3 Acknowledgments This network of mentors, colleagues, friends, and family is simply amazing! Many thanks to... ...My advisor Prof. Fasel for enduring my arguments and crazy ideas about the dynamics of soaring. -
Closing the Loop in Dynamic Soaring
AIAA 2014-0263 AIAA SciTech 13-17 January 2014, National Harbor, Maryland AIAA Guidance, Navigation, and Control Conference Closing the Loop in Dynamic Soaring John J. Bird∗ and Jack W. Langelaany The Pennsylvania State University, University Park, PA 16802 USA Corey Montella,z John Spletzer,x and Joachim Grenestedt{ Lehigh University, Bethlehem, PA 18015 USA This paper examines closed-loop dynamic soaring by small autonomous aircraft. Wind field estimation, trajectory planning, and path-following control are integrated into a sys- tem to enable dynamic soaring. The control architecture is described, performance of components of the architecture is assessed in Monte Carlo simulation, and the trajectory constraints imposed by existing hardware are described. Hardware in the loop simulation using a Piccolo SL autopilot module are used to examine the feasibility of dynamic soaring in the shear layer behind a ridge, and the limitations of the system are described. Results show that even with imperfect path following dynamic soaring is possible with currently existing hardware. The effect of turbulence is assessed through the addition of Dryden turbulence in the simulation environment. I. Introduction For certain missions, such as ocean monitoring, dynamic soaring has the potential to greatly enhance range and endurance of small uavs. Albatrosses and petrels are similar in both size and weight to small unmanned aircraft, and they routinely employ dynamic soaring to travel thousands of kilometers.1,2,3 Deittert et al. show that the probability of winds that permit dynamic soaring by small uavs exceeds 50% in the southern oceans, and this probability is roughly 90% for albatrosses.4 The difference is because albatrosses can descend to very low altitude (dragging a wingtip in the water) and uavs must maintain a significant safety margin. -
Soaring Forecasts: Digging for Data at NWS Web Sites by Dan Shoemaker, NWS Fort Worth, TX
December 2003 National Weather Service Volume 2, Number 3 Soaring Forecasts: Digging For Data at NWS Web Sites by Dan Shoemaker, NWS Fort Worth, TX The National Weather Service (NWS) sphere alone work to keep their refuge from In this Issue: serves a broad base of aviation users that the everyday world aloft. include soaring pilots. The main sources The soaring community is extensive. Soaring Forecasts: of information are TAFs, from Weather One estimate puts the number around Digging For Data Forecast Offices “WFOs”, numerous 20,000 pilots flying sailplanes, hang gliders, products from the Aviation Weather Cen- and paragliders. As a group, these pilots have at NWS Web Sites ter “AWC” and the computer generated had to hone good meteorological sense to Surface Analysis 1 guidance from the National Centers for maximize their soaring experience. It’s worth Environmental Prediction “NCEP”. noting that sailplanes have soared past the Specific NWS Forecast for soaring are tropopause, and hang gliders and paragliders Volcanic Ash: mainly throughout the southwestern por- have reached altitudes above 18,000 ft. Hang Significant Aviation tion of the US. But but we’ll discuss gliders and paragliders routinely make Hazard 5 weather products and information that unpowered cross country trips of more than assist making soaring forecast for other 100 miles. The current hang glider cross locations, as savvy, resourceful soaring pi- country record is over 400 miles. All by tap- lots, hangliders, and paragliders enjoy im- ping the resources of the free air without a mensely the thrill of letting the atmo- powered assist after release. -
Dynamic Soaring: Aerodynamics for Albatrosses
IOP PUBLISHING EUROPEAN JOURNAL OF PHYSICS Eur. J. Phys. 30 (2009) 75–84 doi:10.1088/0143-0807/30/1/008 Dynamic soaring: aerodynamics for albatrosses Mark Denny 5114 Sandgate Road, RR#1, Victoria, British Columbia, V9C 3Z2, Canada E-mail: [email protected] Received 27 August 2008, in final form 1 October 2008 Published 6 November 2008 Online at stacks.iop.org/EJP/30/75 Abstract Albatrosses have evolved to soar and glide efficiently. By maximizing their lift- to-drag ratio L/D, albatrosses can gain energy from the wind and can travel long distances with little effort. We simplify the difficult aerodynamic equations of motion by assuming that albatrosses maintain a constant L/D. Analytic solutions to the simplified equations provide an instructive and appealing example of fixed-wing aerodynamics suitable for undergraduate demonstration. 1. Introduction Albatrosses (figure 1) are among the most pelagic of birds. They nest on remote islands in the ‘Roaring Forties’ and ‘Furious Fifties’, i.e., in the wind-swept southern regions of the Pacific, Atlantic and Indian Oceans that surround Antarctica. They feed primarily upon squid, and roam widely for food to feed their young. A typical albatross feeding trip may take 10 days and cover 1000 km per day. Albatrosses may make half a dozen circumpolar trips each year, taking advantage of the prevailing westerly winds, and adopting characteristic looping flight patterns that best extract energy from the wind. When travelling northward they loop in an anticlockwise direction, and loop clockwise when heading south (we will explain why this is so). Albatrosses are supremely well adapted to this pelagic1 life in the windy southern oceans. -
½ Skydrop User Guide
½ SkyDrop user guide 2102 SkyDrop – combined GPS variometer instant analog/digital vario – no delay response GPS tracklog – IGC, FAI1 Civil approved or KML Bluetooth & USB connectivity – Android, iOS, PC full customizable – multiple screens, layouts and widgets xc navigation functions – optimized route for competitions thermal assistant, airspace warning, wind speed & direction ground speed, altitude above ground, compass, odometer light weight & compact size – 68g, 98 x 58 x 20 mm about this user guide Despite the fact that we made SkyDrop vario as intuitive as possible, we recommend to read this user guide. We know well this is not your favorite activity, so just briefly go through to understand basic concept. You can leave detailed study of every function for winter time or if you want to learn about specific function. You don’t have to keep the printed copy, PDF copy is stored inside vario (SD card), or you can find it on our webpage skybean.eu or vps.skybean.eu buttons long press (for 1s) – turn on, pull up menu bar, move to upper level in menu, toggle widget value, start/stop flight stopwatch, short press – confirm, list adjustable widgets on home screen, turn off device (if menu bar is pulled up), press & hold for 5s to turn device off short press – scroll between home screens to the left, select widget menu if menu bar is pulled up, scroll up in menu, lower value during setting parameter, press & hold to rapid value lowering short press – scroll between home screens to the right, select settings menu if menu bar is pulled up, scroll down in menu, raise value during setting parameter, press & hold to rapid value raising important note – please read SkyDrop is in silent mode after start-up, so if you want to hear vario sound, select FTime widget and manually start the flight by long press. -
1. Check out Your Bird
1. Check out your bird ➢ Where are the feet placed on the body? Measure L Range of values: 47% Hawaiian Petrel (Procellariidae) to Common Murre 74% (Alcidae) 1. Check out your bird ➢ Where are the feet placed on the body? Measure L Range of values: 42% Chicken (Phasianidae) to Western Greebe 100% (Podicipedidae) 1. Check out your bird ➢ What are the feet like ? Write a brief description and make a drawing ➢ What is the tarsus like ? Write a brief description of the cross-section shape (Note: use calipers to measure tarsus cross-section) Tarsus Ratio = Parallel to leg movement Perpendicular to leg movement Round (Wood 1993) Elliptical Tarsus Tarsus 1. Check out your bird Tarsus Ratio = Parallel to leg movement Perpendicular to leg movement Range of values: Values < 1.00 1.00 Black-winged Petrel 0.80 RFBO (Procellariidae) (Sulidae) to to BRBO Common Murre (Sulidae) 1.50 (Alcidae) 0.80 Tarso-metatarsus Section Ratio (Wood 1993) Major and minor axes (a and b) of one tarsus per bird measured with vernier calipers at mid- point between ankle and knee. Cross-section ratio (a / b) reflects the extent to which tarsus is laterally compressed. Leg Position vs Tarsus Ratio 80 COMU 70 BRBO 60 Leg Position SOTEBOPE 50 RFBOBWPE GWGU (% Body Length)(% Body HAPE 40 0.6 0.8 1.0 1.2 1.4 1.6 1.8 2.0 Tarsus Ratio 2. Make Bird Measurements ➢ Weight (to the closest gram): ➢ Lay out bird on its back and stretch the wings out. 2. Make Wing Measurements Wing Span = Wing Chord = Wing Aspect Ratio = Wing Loading = 2.