Design and Navigation of Flying Robots
|
|
|
- Grace Sullivan
- 6 years ago
- Views:
Transcription
1 Design and Navigation of Flying Robots Roland Siegwart, ETH Zurich Drones: From Technology to Policy, Security to Ethics 30 January 2015, ETH Zurich Roland Siegwart ASL ETH Zurich Micro Air Vehicles Walking and Running Quadruped Robots Service Robots Autonomous Robots/Cars for Inner City Environments Inspection Robots Space Robots for Planetary Exploration Swimming Robots
2 UAV (Unmanned Aerial Vehicles) flight concepts Helicopters: < 20 minutes Highly dynamic and agility Fixed Wing Airplanes: > some hours; continuous flights possible Non-holonomic constraints Blimp: lighter-than-air > some hours (dependent on wind conditions); Sensitive to wind Large size (dependent on payload) Flapping wings < 20 minutes; gliding mode possible Non-holonomic constraints Very complex mechanics Festo BionicOpter Roland Siegwart UAV potential applications Search and rescue, surveillance Industrial inspection Agriculture, mining and construction Next generation satellites Roland Siegwart
3 UAV requirements Appropriate flight concept Power autonomy Agility Robustness Navigation with on-board sensing and processing Robustness against communication and GPS loss home button Simple and intuitive operation Stable on hands-off Collision avoidance and localization / SLAM Roland Siegwart UAV requirements Appropriate flight concept Power autonomy Agility Robustness Navigation with on-board sensing and processing Robustness against communication and GPS loss home button Simple and intuitive operation Stable on hands-off Collision avoidance and localization / SLAM Roland Siegwart
4 EU Projects Unmanned Aerial Systems Search and Rescue Transportation (Industrial) Inspection Agriculture Yingxiu, May 15th 2008 Narcea power plant, northern Spain Roland Siegwart Scaling Down of Helicopters OS CoaX mufly cm 650 g 30 cm 200 g 10 cm 50 g Roland Siegwart
![[Leutenegger,Chli,Siegwart 11]](/docs-images/77/76490076/images/5-2.jpg "Roland Siegwart 06.11.")
5 Visual - Inertial SLAM cheap and available ADIS Strong short-term temporal pose constraints + IDS ueye Spatial relative pose constraints Information on structure [Leutenegger,Chli,Siegwart 11] Roland Siegwart UAV Vision only navigation Swarm of small helicopters Vision only navigation (one camera, GPS denied) Fully autonomous with on-board computing Feature-based visual SLAM robust against lighting changes and large scale changes Proto 1 Proto 2 Proto 3 Roland Siegwart
6 A Synchronized Visual-Inertial Sensor System with FPGA Pre-Processing for Accurate Real-Time Slam Roland Siegwart Keyframe VIO with Online Extrinsics Estimation Handheld around ETH MSCKF: visual-inertial stochastic cloning slidingwindow filter (Mourikis et al., 2009). Roland Siegwart
7 UAV collision avoidance and path planning Real time 3D mapping (on-board) optimal path planning considering localization uncertainties Proto 1 Proto 2 Proto 3 Roland Siegwart UAV facade scanning and 3D reconstruction Enhanced teleoperation or autonomous operation Visual-inertial localization for optimal 3D reconstruction Proto 1 Proto 2 Proto 3 Roland Siegwart
8 UAV 3D mapping in mines Vision-based localization and SLAM Laser-based 3D mapping Roland Siegwart Solar Airplane design methodology for continuous flights Based on Mass & Power Balance Need for precise scaling laws (mass models) Airplane Parts Solar cells Battery Airframe Total mass Aerodynamic & Conditions Power for level Flight Roland Siegwart
![Solar Airplane Optimization Design space at 38 N, June 21 st Battery mass [kg] Fixed Aspect Ratio: 18.5 12 10 8 6 4 2 Excess Time [h] 0 3 4 5 6 7 8 9 Wingspan [m] Flat optimum at wingspan 11.](/docs-images/77/76490076/images/9-0.jpg "5 m 15 10 5 0 Chosen AtlantikSolar configuration: Wingspan 5.65 m Battery mass 2.9 kg Structural weight Predicted: 1 317 g Effective: 1 800 g Prediction [Noth 08]: 4 638 g Roland Siegwart 06.11.")
9 Solar Airplane Optimization Design space at 38 N, June 21 st Battery mass [kg] Fixed Aspect Ratio: Excess Time [h] Wingspan [m] Flat optimum at wingspan 11.5 m Chosen AtlantikSolar configuration: Wingspan 5.65 m Battery mass 2.9 kg Structural weight Predicted: g Effective: g Prediction [Noth 08]: g Roland Siegwart Solar powered fixed wing airplanes: Long duration / continuous flights sensesoar Wingspan: 3 m Wing area: m2 Peak Solar power 140 W Power Consumption 50 W Masses: Overall: 3.72 kg Batteries: 1.89 kg Nominal Speed 10 m/s Sensors Air speed IMU GPS Camera IR camera AtlantikSolar Wingspan: 5.64 m Solar area: 1.5 m2 Peak Solar power 280 W Power Consumption 40 W Masses: Overall: 6.2 kg Batteries: 2.9 kg Nominal Speed 10 m/s Sensors Air speed IMU GPS Camera Roland Siegwart
10 crossing the Atlantic in summer 2015 Boston Lisbon Around 6 days without tail wind Roland Siegwart Solar Airplane visual navigation Visual-inertial sensor with multiple cameras Integrated thermal vision Robust state estimation and flight control Autonomous planning for complete inspection Long endurance solar powered fight Roland Siegwart
11 ASL Team Roland Siegwart
Le développement technique des véhicules autonomes
Shaping the future Le développement technique des véhicules autonomes Renaud Dubé, Roland Siegwart, ETH Zurich www.asl.ethz.ch www.wysszurich.ch Fribourg, 23 Juin 2016 Renaud Dubé 23.06.2016 1 Content
Case Studies: Design of Solar Powered Airplanes
Case Studies: Design of Solar Powered Airplanes Philipp Oettershagen, philipp.oettershagen@mavt.ethz.ch Fixed Wing UAS: Control and Fuel Case Studies 23.11.2015 14 Introduction: Why Solar Powered Flight?
In recent years, multirotor helicopter type autonomous UAVs are being used for aerial photography and aerial survey. In addition, various
25 6 18 In recent years, multirotor helicopter type autonomous UAVs are being used for aerial photography and aerial survey. In addition, various applications such as buildings maintenance, security and
FLYING CAR NANODEGREE SYLLABUS
FLYING CAR NANODEGREE SYLLABUS Term 1: Aerial Robotics 2 Course 1: Introduction 2 Course 2: Planning 2 Course 3: Control 3 Course 4: Estimation 3 Term 2: Intelligent Air Systems 4 Course 5: Flying Cars
In 2003, A-Level Aerosystems (ZALA AERO) was founded by current company President Alexander Zakharov, since then he has led
A-Level Aerosystems In 2003, A-Level Aerosystems (ZALA AERO) was founded by current company President Alexander Zakharov, since then he has led the company to be a leader in the micro UAV market in Russian
Small UAV A French MoD perspective and planning
Small UAV A French MoD perspective and planning French ISTAR segmentation portable transportable infrastructure System volume Tactical Small UAV Contact Combat Helicopters (MTI) Fighter Aircrafts Land
9/11/2018. UAS110 Intro to UAV Systems. UAS110 Intro to Unmanned Aerial Systems. Overview. Impetus. 3: UAV Classification
UAS110 Intro to Unmanned Aerial Systems 2018 J. Sumey California University of PA rev. 9/11/18 Overview UAVs may be classified according to various metrics scale (size) method of lift generation range/endurance
STUDYING THE POSSIBILITY OF INCREASING THE FLIGHT AUTONOMY OF A ROTARY-WING MUAV
SCIENTIFIC RESEARCH AND EDUCATION IN THE AIR FORCE AFASES2017 STUDYING THE POSSIBILITY OF INCREASING THE FLIGHT AUTONOMY OF A ROTARY-WING MUAV Cristian VIDAN *, Daniel MĂRĂCINE ** * Military Technical
Content. Introduction. Technology. Type of unmanned vehicle. Past, Present, Future. Conclusion
Introduction Content Technology Type of unmanned vehicle Past, Present, Future Conclusion What is unmanned vehicles? l Without a person on board l Remote controlled l Remote guided vehicles Reduce casualty
Unmanned Air Vehicles (UAVs): Classification, Legislation and Future applications Presenter: Dr-Ing Dimitrios E. Mazarakos
Unmanned Air Vehicles (UAVs): Classification, Legislation and Future applications Presenter: Dr-Ing Dimitrios E. Mazarakos The presenter Dr-Ing Dimitrios E. Mazarakos Dipl. in Mechanical Engineering and
A brief History of Unmanned Aircraft
A brief History of Unmanned Aircraft Technological Background Dr. Bérénice Mettler University of Minnesota Jan. 22-24, 2012 (v. 1/15/13) Dr. Bérénice Mettler (University of Minnesota) A brief History of
SENSITIVITY ANALYSIS OF DESIGN PARAMETERS OF A SMALL SOLAR-POWERED ELECTRIC UNMANNED AERIAL VEHICLE
Journal of Engineering Science and Technology Vol. 13, No. 12 (2018) 3922-3931 School of Engineering, Taylor s University SENSITIVITY ANALYSIS OF DESIGN PARAMETERS OF A SMALL SOLAR-POWERED ELECTRIC UNMANNED
FLYEYE Unmanned Aerial System
FLYEYE Unmanned Aerial System FLYEYE Unmanned Aerial System About Flytronic FLYTRONIC is a dynamic modern engineering company focussed on developing Unmanned Aerial Systems to provide observation and reconnaissance
UAV KF-1 helicopter. CopterCam UAV KF-1 helicopter specification
UAV KF-1 helicopter The provided helicopter is a self-stabilizing unmanned mini-helicopter that can be used as an aerial platform for several applications, such as aerial filming, photography, surveillance,
SURVEYOR-H. Technical Data. Max speed 120 km/h. Engine power 7.2 hp. Powerplant Modified Zenoah G29E. Fuel tank volume 3.6 l
rev. 28.10.14 * features & specifications are subject to change without notice. Technical Data Max speed 120 km/h Engine power 7.2 hp Powerplant Modified Zenoah G29E Fuel tank volume 3.6 l Payload with
THE FALCON REDUNDANCY HIGH WIND TOLERANCE BEST USED FOR SURVEILLANCE & SECURITY DELIVERY & TRANSPORT
THE FALCON REDUNDANCY HIGH WIND TOLERANCE The Falcon's new air frame and motor configuration is the new best in its class of light payloads with flight times of up to 50 minutes. This makes the Falcon
DRONE & UAV.
www.erapkorea.co.kr DRONE & UAV Extended flight time Proven to be reliable, safe and easy to use Various fields of operation Completely autonomous, and manually controlled ERAP DRONE & UAV WHY ERAP s MAPPING
Initial Concept Review Team Alpha ALUM Rover (Astronaut Lunar Utility Mobile Rover) Friday, October 30, GMT
Initial Concept Review Team Alpha ALUM Rover (Astronaut Lunar Utility Mobile Rover) Friday, October 30, 2009 1830-2030 GMT Rover Requirements/Capabilities Performance Requirements Keep up with an astronaut
High aspect ratio for high endurance. Mechanical simplicity. Low empty weight. STOVL or STOL capability. And for the propulsion system:
Idealized tilt-thrust (U) All of the UAV options that we've been able to analyze suffer from some deficiency. A diesel, fixed-wing UAV could possibly satisfy the range and endurance objectives, but integration
Mobile Robots Introduction and Lecture Overview
ASL Autonomous Systems Lab Mobile Robots Introduction and Lecture Overview Autonomous Mobile Robots Roland Siegwart Margarita Chli, Paul Furgale, Marco Hutter, Martin Rufli, Davide Scaramuzza Autonomous
Cooperative EVA/Telerobotic Surface Operations in Support of Exploration Science
Cooperative EVA/Telerobotic Surface Operations in Support of Exploration Science David L. Akin http://www.ssl.umd.edu Planetary Surface Robotics EVA support and autonomous operations at all physical scales
Tactical Technology Office. Tactical Technology Office. Programs. DARPATech 2000 Dr. David Whelan Director Whelan Darpatech
Programs DARPATech 2000 Dr. David Whelan Director dwhelan@darpa.mil Global Surveillance Land Systems Aerospace Systems Embedded Processing & Control Global Surveillance Objectives: Birth-to-Death Track
Fire Fighting Equipment Development - Unmanned Aerial Vehicle Trials. Ripley Valley Rural Fire Brigade - August 2010
Fire Fighting Equipment Development - Unmanned Aerial Vehicle Trials Ripley Valley Rural Fire Brigade - August 2010 The Brigade offered to help evaluate the capabilities of an Unmanned Aerial Vehicle (UAV)
Solar Based Propulsion System UAV Conceptual Design ( * )
Solar Based Propulsion System UAV Conceptual Design ( * ) Avi Ayele*, Ohad Gur, and Aviv Rosen* *Technion Israel Institute of Technology IAI Israel Aerospace Industries (*) Ayele A., Gur O., Rosen A.,
UAV Fuel Cell Module. Fly. Longer. Fly. Further. Achieve More
UAV Fuel Cell Module Fly Longer Fly Further Achieve More The use of professional Unmanned Aerial Vehicles (UAVs) has grown significantly in recent years. Owing to the constraints of traditional battery
Control of Mobile Robots
Control of Mobile Robots Introduction Prof. Luca Bascetta (luca.bascetta@polimi.it) Politecnico di Milano Dipartimento di Elettronica, Informazione e Bioingegneria Applications of mobile autonomous robots
Autonomous inverted helicopter flight via reinforcement learning
Autonomous inverted helicopter flight via reinforcement learning Andrew Y. Ng, Adam Coates, Mark Diel, Varun Ganapathi, Jamie Schulte, Ben Tse, Eric Berger, and Eric Liang By Varun Grover Outline! Helicopter
An Overview of CSA s s Space Robotics Activities
An Overview of CSA s s Space Robotics Activities Erick Dupuis, Mo Farhat ASTRA 2011 ESTEC, Noordwijk, The Netherlands Introduction Key Priority Area for CSA Recent Reorganisation Strategy Guided by Global
Design and Simulation of New Versions of Tube Launched UAV
21st International Congress on Modelling and Simulation, Gold Coast, Australia, 29 Nov to 4 Dec 2015 www.mssanz.org.au/modsim2015 Design and Simulation of New Versions of Tube Launched UAV Y. Zhou and
PENGUIN C UAS OPERATIONS & MAINTENANCE TRAINING 20 HOURS FLIGHT ENDURANCE 100KM RANGE ITAR - FREE CREW OF TWO
PENGUIN C UAS LONG ENDURANCE UNMANNED AERIAL SYSTEM 20 HOURS FLIGHT ENDURANCE OPERATIONS & MAINTENANCE TRAINING 100KM RANGE ITAR - FREE CREW OF TWO U AV FAC T O RY LT D., E U R O P E U AV FAC T O RY U
Development of an Extended Range, Large Caliber, Modular Payload Projectile
1 Development of an Extended Range, Large Caliber, Modular Payload Projectile April 12th, 2011 Miami, Florida, USA 46 th Annual Gun & Missile Systems Conference & Exhibition Speaker: Pierre-Antoine Rainville
DSSI UAV. Unmanned Aerial Vehicle. Research & Development Project
UAV Unmanned Aerial Vehicle HISTORY AND SKILLS of Small UAV with electrically powered propeller Description of the solution: Airframe,electronics, 2 battery sets 1 spare Airframe, battery charger Transport
Eurathlon Scenario Application Paper (SAP) Review Sheet
Scenario Application Paper (SAP) Review Sheet Team/Robot Scenario FKIE Reconnaissance and surveillance in urban structures (USAR) For each of the following aspects, especially concerning the team s approach
Unmanned Surface Vessels - Opportunities and Technology
Polarconference 2016 DTU 1-2 Nov 2016 Unmanned Surface Vessels - Opportunities and Technology Mogens Blanke DTU Professor of Automation and Control, DTU-Elektro Adjunct Professor at AMOS Center of Excellence,
AT-10 Electric/HF Hybrid VTOL UAS
AT-10 Electric/HF Hybrid VTOL UAS Acuity Technologies Robert Clark bob@acuitytx.com Summary The AT-10 is a tactical size hybrid propulsion VTOL UAS with a nose camera mount and a large payload bay. Propulsion
Powertrain Design for Hand- Launchable Long Endurance Unmanned Aerial Vehicles
Powertrain Design for Hand- Launchable Long Endurance Unmanned Aerial Vehicles Stuart Boland Derek Keen 1 Justin Nelson Brian Taylor Nick Wagner Dr. Thomas Bradley 47 th AIAA/ASME/SAE/ASEE JPC Outline
UAV Fuel Cell Power Module. Fly. Longer. Fly. Further. Achieve More
UAV Fuel Cell Power Module Fly Longer Fly Further Achieve More The use of professional Unmanned Aerial Vehicles (UAVs) has grown significantly in recent years. Owing to the constraints of traditional battery
Prototyping Collision Avoidance for suas
Prototyping Collision Avoidance for Michael P. Owen 5 December 2017 Sponsor: Neal Suchy, FAA AJM-233 DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. Trends in Unmanned
UAV for participatory mapping in Haiti
UAV for participatory mapping in Haiti OpenStreetMap - OSM www.openstreetmap.org Use of GPS and satellite imagery (Bing) to build the map History January 12 th, 2010 : earthquake - intensity 7 230 000
UAV Systems Comparison. Planes, Frames and Autopilots
UAV Systems Comparison Planes, Frames and Autopilots Presenter: Robert Lefebvre BASc Mechanical Engineering, University of Ottawa Managing Director NOVAerial Robotics Inc. Ardupilot Developer 6 Years UAV
Self-Driving Vehicles in the Park
Self-Driving Vehicles in the Park Bryant Walker Smith Center for Internet and Society Center for Automotive Research cyberlaw.stanford.edu/about/people/bryant-walker-smith 1 A robot by any other name Self-driving
MAV and UAV Research at Rochester Institute of Technology. Rochester Institute of Technology
MAV and UAV Research at Andrew Streett 5 th year BS/MS Student 2005-2006 MAV Team Lead Jason Grow BS/MS Graduate of RIT 2003-2004 MAV Team Lead Boeing Phantom Works, HB 714-372-9026 jason.a.grow@boeing.com
COLLISION AVOIDANCE OF INDOOR FLYING DOUBLE TETRAHEDRON HEXA-ROTORCRAFT
8 TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES COLLISION AVOIDANCE OF INDOOR FLYING DOUBLE TETRAHEDRON HEXA-ROTORCRAFT Takehiro HIGUCHI*, Daichi TORATANI**, and Seiya UENO* *Faculty of Environment
Innovating the future of disaster relief
Innovating the future of disaster relief American Helicopter Society International 33rd Annual Student Design Competition Graduate Student Team Submission VEHICLE OVERVIEW FOUR VIEW DRAWING INTERNAL COMPONENTS
Seventh Framework Programme THEME: AAT Breakthrough and emerging technologies Call: FP7-AAT-2012-RTD-L0 AGEN
Seventh Framework Programme THEME: AAT.2012.6.3-1. Breakthrough and emerging technologies Call: FP7-AAT-2012-RTD-L0 AGEN Atomic Gyroscope for Enhanced Navigation Grant agreement no.: 322466 Publishable
Data acquisition within T-AI DSS
Data acquisition within T-AI DSS Tamara Ivelja 1, Ivan Racetin¹, Andrija Krtalic¹ Abstract The module of T-AI DSS for data acquisition should provide the stability and reliability of (aerial) data acquisition
Electric Penguin s philosophy:
UNMANNED PLATFORMS AND SUBSYSTEMS Datasheet v 1.1 Penguin BE Electric Unmanned Platform Up to 110 minutes of endurance 2 with 2.8 kg payload 23 liters of payload volume Quick replaceable battery cartridge
Super Squadron technical paper for. International Aerial Robotics Competition Team Reconnaissance. C. Aasish (M.
Super Squadron technical paper for International Aerial Robotics Competition 2017 Team Reconnaissance C. Aasish (M.Tech Avionics) S. Jayadeep (B.Tech Avionics) N. Gowri (B.Tech Aerospace) ABSTRACT The
Analysts/Fund Managers Visit 19 April Autonomous Systems and Future Capability Mark Kane
Analysts/Fund Managers Visit 19 April 2007 Autonomous Systems and Future Capability Mark Kane The Rationale for UAVs The Rationale for UAVs UAVs generally seen to carry out the dull, dirty, and dangerous
UAV Drones. Team RamRod: Tyler Barry James Bohn Daniel Ramirez Hari Shrestha Arlo Swanson Garret Wilbanks
UAV Drones Team RamRod: Tyler Barry James Bohn Daniel Ramirez Hari Shrestha Arlo Swanson Garret Wilbanks Outline Introduction History Technology and Applications Current Future Economics and Marketability
komatsu.com.au komatsu.co.nz /KomatsuAustralia/
INNOVATIVE INTELLIGENT INTEGRATED komatsu.com.au komatsu.co.nz /KomatsuAustralia/ intelligent MACHINE CONTROL Introducing intelligent Machine Control Komatsu s innovative intelligent Machine Control (imc)
suas in CAP Delaware Wing HQ, Civil Air Patrol Development of small Unmanned Aerial Systems
Delaware Wing HQ, Civil Air Patrol suas in CAP Development of small Unmanned Aerial Systems Advent of the suas Small Unmanned Aerial Systems have become very common recently Sophisticated microprocessors
Helicopter Experience, Date: August 1-6 Location: Central Connecticut State University
Helicopter Experience, 2010 Date: August 1-6 Location: Central Connecticut State University 1 Out Line Schedule Selection Process What students will receive 2 com For All Details 3 Sunday, August 1, 2010,
Design and Fabrication of UAV (Unmanned Aerial Vehicle)
Design and Fabrication of UAV (Unmanned Aerial Vehicle) B.V.Ramanjaneyulu Associate Professor, M.V.S.E Pavan Kumar CH.Sambhu Prasad M.Balaji Abstract: The use of autonomous vehicles, for a wide variety
Towards the Optimisation of. Adaptive Aeroelastic Structures
Towards the Optimisation of Jonathan Cooper Mike Amprikidis, Vijaya Hodere, Gareth Vio School of Mechanical, Aerospace and Civil Engineering University of Manchester ERCOFTAC 6th April 2006 Contents Introduction
LiDAR and the Autonomous Vehicle Revolution for Truck and Ride Sharing Fleets
July 12, 2017 LiDAR and the Autonomous Vehicle Revolution for Truck and Ride Sharing Fleets Louay Eldada CEO and Co-founder, Quanergy Systems New Paradigm in 3D Sensing Disruptive Technologies: Solid State
ParcelBot A Tracked Parcel Transporter with High Obstacle Negotiation Capabilities
Research Collection Conference Paper ParcelBot A Tracked Parcel Transporter with High Obstacle Negotiation Capabilities Author(s): Hoepflinger, Mark H.; Baschung, David; Remy, C. D.; Hutter, Marco; Siegwart,
Part II. HISTORICAL AND ENGINEERING ANALYSIS OF AIRSHIP PLAN-AND- DESIGN AND SERVICE DECISIONS
CONTENTS MONOGRAPHER S FOREWORD DEFENITIONS, SYMBOLS, ABBREVIATIONS, AND INDICES Part I. LAWS AND RULES OF AEROSTATIC FLIGHT PRINCIPLE Chapter 1. AIRCRAFT FLIGHT PRINCIPLE 1.1 Flight Principle Classification
Dr. D. Feszty RUAS Project Manager (CB 3207) Jen Gatenby RUAS Project Integrator ( )
February 7 th, 2014 RUAS: Capstone Design Project Team Carleton University 1125 Colonel By Drive K1S 5B6 Carleton University Engineering Student Equipment Fund Dept. of Engineering & Design Office of the
DELHI TECHNOLOGICAL UNIVERSITY TEAM RIPPLE Design Report
DELHI TECHNOLOGICAL UNIVERSITY TEAM RIPPLE Design Report May 16th, 2018 Faculty Advisor Statement: I hereby certify that the development of vehicle, described in this report has been equivalent to the
University of Central Florida Entry for the 2013 AUVSI Foundation s International Aerial Robotics Competition
University of Central Florida Entry for the 2013 AUVSI Foundation s International Aerial Robotics Competition Logan Camacho University of Central Florida, Aerospace Engineering Karl Ravago University of
Modeling, Structural & CFD Analysis and Optimization of UAV
Modeling, Structural & CFD Analysis and Optimization of UAV Dr Lazaros Tsioraklidis Department of Unified Engineering InterFEA Engineering, Tantalou 7 Thessaloniki GREECE Next Generation tools for UAV
REU: Improving Straight Line Travel in a Miniature Wheeled Robot
THE INSTITUTE FOR SYSTEMS RESEARCH ISR TECHNICAL REPORT 2013-12 REU: Improving Straight Line Travel in a Miniature Wheeled Robot Katie Gessler, Andrew Sabelhaus, Sarah Bergbreiter ISR develops, applies
Introduction Projects Basic Design Perception Motion Planning Mission Planning Behaviour Conclusion. Autonomous Vehicles
Dipak Chaudhari Sriram Kashyap M S 2008 Outline 1 Introduction 2 Projects 3 Basic Design 4 Perception 5 Motion Planning 6 Mission Planning 7 Behaviour 8 Conclusion Introduction Unmanned Vehicles: No driver
UAV Fuel Cell Module. Fly. Longer. Fly. Further. Achieve More
UAV Fuel Cell Module Fly Longer Fly Further Achieve More The use of professional Unmanned Aerial Vehicles (UAVs) has grown significantly in recent years. Owing to the constraints of traditional battery
Eurathlon Scenario Application Paper (SAP) Review Sheet
Scenario Application Paper (SAP) Review Sheet Team/Robot Scenario FKIE Autonomous Navigation For each of the following aspects, especially concerning the team s approach to scenariospecific challenges,
Jay Gundlach AIAA EDUCATION SERIES. Manassas, Virginia. Joseph A. Schetz, Editor-in-Chief. Blacksburg, Virginia. Aurora Flight Sciences
Jay Gundlach Aurora Flight Sciences Manassas, Virginia AIAA EDUCATION SERIES Joseph A. Schetz, Editor-in-Chief Virginia Polytechnic Institute and State University Blacksburg, Virginia Published by the
Hybrid VTOL: Increased Energy Density for Increased Payload and Endurance
Hybrid VTOL: Increased Energy Density for Increased Payload and Endurance Top Flight Airborg 10K H8 with Micro Hybrid Generator Engine Dr. Paul DeBitetto, VP/Software Engineering, paul.debitetto@topflighttech.com,
Active Driver Assistance for Vehicle Lanekeeping
Active Driver Assistance for Vehicle Lanekeeping Eric J. Rossetter October 30, 2003 D D L ynamic esign aboratory Motivation In 2001, 43% of all vehicle fatalities in the U.S. were caused by a collision
Sciences for Maneuver Campaign
Mr. Eric Spero Sciences for Maneuver Campaign U.S. Army Research Laboratory Ground Air Sciences for Maneuver Campaign Science & Technology enabled air and ground platform capabilities to significantly
Aeronautical Systems Center
Aeronautical Systems Center Global Hawk Program Overview Michael Johnston 303 AESG/LG DSN: 787-4047 Comm: 937-255-4047 michael.johnston@wpafb.af.mil RQ-4A Global Hawk System Global Hawk: High-altitude,
AN ANALYSIS OF THE STABILITY AND PERFORMANCES OF ROTARY WING MICRO AERIAL VEHICLES
AN ANALYSIS OF THE STABILITY AND PERFORMANCES OF ROTARY WING MICRO AERIAL VEHICLES Pavel NEČAS*, Ionică CÎRCIU**, Constantin ROTARU***, Mircea BOŞCOIANU** *Armed Forces Academy of General Milan Rastislav
Presse-Information. The mycopter project points the way towards Personal Aerial Vehicles
The mycopter project points the way towards Personal Aerial Vehicles Road congestion is a fact of everyday life for many people. A possible solution for the future is expanding personal transport to include
TABLE OF CONTENTS. Thank you for your interest in CUAir
SPONSORSHIP INFORMATION 2018-2019 TABLE OF CONTENTS The Team Subteams The Competition Theia II Accomplishments 2019 Air System Outreach Why Contribute Sponsorship Levels 2017-2018 Sponsors Contact Us 3
Investigative Technologies and Techniques
Investigative Technologies and Techniques Using Drones In Accident Investigation (Aerial Photography) Drone used in accident investigation Technical specifications and performance Flat 8 motor configuration
Autonomous Quadrotor for the 2014 International Aerial Robotics Competition
Autonomous Quadrotor for the 2014 International Aerial Robotics Competition Yongseng Ng, Keekiat Chua, Chengkhoon Tan, Weixiong Shi, Chautiong Yeo, Yunfa Hon Temasek Polytechnic, Singapore ABSTRACT This
CENTAUR OPTIONALLY-PILOTED AIRCRAFT ULTIMATE FLEXIBILITY FOR AIRBORNE SENSING
CENTAUR OPTIONALLY-PILOTED AIRCRAFT ULTIMATE FLEXIBILITY FOR AIRBORNE SENSING CENTAUR A NEW LEVEL OF OPERATIONAL FLEXIBILITY Aurora Flight Sciences Centaur combines the best of manned and unmanned surveillance
UDC (045) Łukasz Sawicki, Jacek Widziszowski, Norman Płaskociński State School of Higher Education in Chelm, Poland
Наука і молодь. Прикладна серія 7 UDC 629.047 (045) Łukasz Sawicki, Jacek Widziszowski, Norman Płaskociński State School of Higher Education in Chelm, Poland THE GENERAL AIMS OF CONSRTUCTING UAVs The work
Length Height Rotor Diameter Tail Rotor Diameter..12. Tail Boom Length Width
2.1 Air Vehicle 2.1.1 Vehicle General Description The PA-01 Vapor S-UAV is a rotary wing small unmanned aerial vehicle. The AV is powered by an outrunner 8.5hp class brushless electric motor. The airframe
CS 188: Artificial Intelligence
CS 188: Artificial Intelligence Advanced Applications: Robotics Pieter Abbeel UC Berkeley A few slides from Sebastian Thrun, Dan Klein 2 So Far Mostly Foundational Methods 3 1 Advanced Applications 4 Autonomous
Control of a Coaxial Helicopter with Center of Gravity Steering
Control of a Coaxial Helicopter with Center of Gravity Steering Christian Bermes, Kevin Sartori, Dario Schafroth, Samir Bouabdallah, and Roland Siegwart {bermesc,ksartori,sdario,samirbo,rsiegwart}@ethz.ch
INSTYTUT TECHNICZNY WOJSK LOTNICZYCH Air Force Institute of Technology
1953-2014 INSTYTUT TECHNICZNY WOJSK LOTNICZYCH Air Force Institute of Technology 01 Aircraft Engines Division Airworthiness Division IT Logistics Support Systems Division Aeroplanes & Helicopters Division
A VERY UNIQUE UAV FLAMINGO MK1 UAV Silvertone Electronics Australia
A VERY UNIQUE UAV FLAMINGO MK1 UAV 01 DESIGN BACKGROUND The design was born out of a perceived need for a low capital cost, surveillance tool for large Farm/ Property owners. 02 SIZE AND WEIGHT The size,
A SOLAR POWERED UAV. 1 Introduction. 2 Requirements specification
A SOLAR POWERED UAV Students: R. al Amrani, R.T.J.P.A. Cloosen, R.A.J.M. van den Eijnde, D. Jong, A.W.S. Kaas, B.T.A. Klaver, M. Klein Heerenbrink, L. van Midden, P.P. Vet, C.J. Voesenek Project tutor:
A COMMERCIAL OF THE SHELF COMPONENTS FOR A UNMANNED AIR VEHICLE PHOTOGRAMMETRY
Section Name A COMMERCIAL OF THE SHELF COMPONENTS FOR A UNMANNED AIR VEHICLE PHOTOGRAMMETRY Pawel Burdziakowski Jakub Szulwic Faculty of Civil and Environmental Engineering, Gdansk University of Technology,
Design and Development of Multi Ornithopter using Bio-mimic Method and Analysis
International Journal of Engineering Research and Technology. ISSN 0974-3154 Volume 6, Number 5 (2013), pp. 593-604 International Research Publication House http://www.irphouse.com Design and Development
MINI-REIS A FAMILY OF MULTIFUNCTIONAL UNMANNED LIGHT JET AIRCRAFTS
National Aerospace University Kharkiv Aviation Institute KhAI Public Joint Stock Company "Kyiv Radio Plant" Inter-Industry Scientific & Research Institute of the Problems of Aircraft Flight Mode Physical
UNIVERSITÉ DE MONCTON FACULTÉ D INGÉNIERIE. Moncton, NB, Canada PROJECT BREAKPOINT 2015 IGVC DESIGN REPORT UNIVERSITÉ DE MONCTON ENGINEERING FACULTY
FACULTÉ D INGÉNIERIE PROJECT BREAKPOINT 2015 IGVC DESIGN REPORT UNIVERSITÉ DE MONCTON ENGINEERING FACULTY IEEEUMoncton Student Branch UNIVERSITÉ DE MONCTON Moncton, NB, Canada 15 MAY 2015 1 Table of Content
PENGUIN B UAV PLATFORM
UNMANNED PLATFORMS AND SUBSYSTEMS Datasheet v.0 PENGUIN B UAV PLATFORM Penguin B platform ready for payload and autopilot integration 0+ hour endurance Fuel injected engine option Up to 10 kg payload capacity
ROBUST AIRFRAME FOR UAV FLIGHT TESTING FOR SALE!
ROBUST AIRFRAME FOR UAV FLIGHT TESTING FOR SALE! My team specializes in fabricating airframes that s appropriate for testing unmanned aerial vehicle components. Our airframes are made of hybrid composite
GEO-7851 USING UAVS TO INCREASE PRODUCTIVITY AND SAFETY IN THE CONSTRUCTION INDUSTRY. Emmanuel de Maistre
GEO-7851 USING UAVS TO INCREASE PRODUCTIVITY AND SAFETY IN THE CONSTRUCTION INDUSTRY Emmanuel de Maistre Better data. Better decisions. Using UAVs to increase productivity and safety in the construction
Robot mobili e tecnologie marine del centro ISME. Alessandro Ridolfi Dipartimento di Ingegneria Industriale Università di Firenze nodo ISME
Robot mobili e tecnologie marine del centro ISME Alessandro Ridolfi Dipartimento di Ingegneria Industriale Università di Firenze nodo ISME NATIONAL INTER-UNIVERSITY CENTER TO SUPPORT RESEARCH ACTIVITIES
Marine Robotics. Alfredo Martins. Unmanned Autonomous Vehicles in Air Land and Sea Politecnico Milano June 2016
Marine Robotics Unmanned Autonomous Vehicles in Air Land and Sea Politecnico Milano June 2016 INESC TEC / ISEP Portugal alfredo.martins@inesctec.pt Multiple autonomous vehicles at sea 2 Multiple coordinated
Smart Control for Electric/Autonomous Vehicles
Smart Control for Electric/Autonomous Vehicles 2 CONTENTS Introduction Benefits and market prospective How autonomous vehicles work Some research applications TEINVEIN 3 Introduction What is the global
UNCLASSIFIED FY 2017 OCO. FY 2017 Base
Exhibit R-2, RDT&E Budget Item Justification: PB 2017 Air Force Date: February 2016 3600: Research, Development, Test & Evaluation, Air Force / BA 2: Applied Research COST ($ in Millions) Prior Years FY
Aerial robots that interact with the environment
Aerial robots that interact with the environment Guillermo Heredia*, Aníbal Ollero * Professor at University of Seville, Spain Robotics, Vision and Control group (GRVC) guiller@us.es Robotics, Vision and
BY HOEYCOMB AEROSPACE TECHNOLOGIES. HC-330 HYBRID-POWERED ALL- ELECTRICITY DRIVEN four-rotor UAV
BY HOEYCOMB AEROSPACE TECHNOLOGIES HC-330 HYBRID-POWERED ALL- ELECTRICITY DRIVEN four-rotor UAV Content SYSTEM SPECIFICATI- ON TYPICAL USING PROCESS OVERVIEW SUBSYSTEM SPECIFICATI- ON 1 OVERVIEW System
Development of a Variable Stability, Modular UAV Airframe for Local Research Purposes
Development of a Variable Stability, Modular UAV Airframe for Local Research Purposes John Monk Principal Engineer CSIR, South Africa 28 October 2008 Outline A Brief History of UAV Developments at the
Design and Development of the UTSA Unmanned Aerial System ACE 1
Design and Development of the UTSA Unmanned Aerial System ACE 1 For use in the 2010 AUVSI Student UAS Competition Ilhan Yilmaz Department of Mechanical Engineering (Team Lead) Christopher Weldon Department
DESIGN AND DEVELOPMENT OF A MICRO AIR VEHICLE (µav) CONCEPT: PROJECT BIDULE
DESIGN AND DEVELOPMENT OF A MICRO AIR VEHIE (µav) CONCEPT: PROJECT BIDULE Mr T. Spoerry, Dr K.C. Wong School of Aerospace, Mechanical and Mechatronic Engineering University of Sydney NSW 6 Abstract This