AT 209 Introduction to Civil Unmanned Aerial Systems (UAS)

Slides:



Advertisements
Similar presentations
A Shared Vision for Arizonas UAS Community Prescott, AZ September 9, 2011 Barry Albrecht CEO Central Arizona Regional Economic Development.
Advertisements

Company Presentation.
Casa RPAS regulatory Development
AirShip V2 VTOL UAV Patent Pending
Waterloo Aerial Robotics Group WARG Mandate: The Waterloo Aerial Robotics Group is a team of University of Waterloo students who, with the support of our.
MicroCART Micro processor C ontrolled A erial R obotics T eam Abstract MicroCART is a group of EE/CprE students tasked with developing an autonomous helicopter.
 PROFESSOR KUNG  GROUP MEMBERS: JEEVEN HUGH, AARON KELLEY, AKRAM GERIES, BRAD LONG, MICHAEL LADAS.
ODS3F –Observation and Detection Systems For Forest Fire Monitoring
Daniel Graves –Project Lead James Reepmeyer – Lead Engineer Brian Smaszcz– Airframe Design Alex Funiciello – Airfoil Design Michael Hardbarger – Control.
MnGeo Statewide Geospatial Advisory Council Hot Topics May 30, 2012 Drones, UAV’s, UAS’s.
Team 6: Autonomous Aerial Vehicle Team Members Department of Mechanical Engineering: Ken Anderson, Arielle Duen, Eric Milo, Ernandes Nascimento and Matthew.
Vertical Launch UAV Project Plan. ∞ Construct an unmanned aerial vehicle (UAV) with a camera payload ∞ UAV must autonomously navigate with real-time video.
Range (nm) Payload (kg) Payload (lb) Endurance (hr) As a total system, Vigilante.
INNOCON Innovative solutions to the modern real time Arial surveillance challenges.
P09233 Flight Parameter Measurements Michael Skube P09233
Automatic Control & Systems Engineering Autonomous Systems Research Mini-UAV for Urban Environments Autonomous Control of Multi-UAV Platforms Future uninhabited.
Electrical and Computer Systems Engineering Postgraduate Student Research Forum 2001 Design and Development of a Distributed Avionics System for use in.
6th Framework Programme Thematic Priority Aeronautics and Space.
Sense & Avoid for UAV Systems
Aerospace Engineering By Patrick Ferrell. Aerospace Engineering is the main branch of engineering concerned with the research, design, development, construction,
New Applications of UAVs – A Driving Force Behind Joint Ventures Presented by; Haider Ali Bhatty Deputy Director General, Advanced Engineering Research.
Μ - CART Microprocessor – Controlled Aerial Robotics Team (Ongo03) An Ongoing Senior Design Project Department of Electrical and Computer Engineering Iowa.
Introduction to Remotely Operated Vehicles ROVs
SWFSC Antarctic UAS Mission Briefing Wayne Perryman, Jefferson Hinke and Douglas Krause.
A New Method for the Tele-operation of Aircraft Dr. Paul Oh James Hing.
UAV for Surveyors and Spatial Analysts An emerging technology for the Geospatial Industry Warren Eade– Mapping and Mobile Manager.
Unmanned aerial systems, what they are and what is available? Professor Sandor M Veres University of Sheffield.
Unmanned Aerial Vehicles “Drones”
Drone Programming Eleanor Roosevelt High School Chin-Sung Lin.
1.  The Autonomous Helicopter Navigation System 2010 is focused on developing a helicopter system capable of autonomous control, navigation and localising.
DARPA ARES Program Ken Dorsett 25October 2014.
Massachusetts Institute of Technology 4 April 2003
Law Enforcement UAS Concept of Operations US Forest Service Law Enforcement & Investigations DRAFT.
AEM 5333 UAV Search and Surveillance. Mission Description Overhead surveillance and tracking – Humans on foot – Moving vehicles Onboard GPS transceiver.
BQM-167A Advanced UAV System Architecture
Federal Aviation Administration 0 Certification Standards for New Technologies June 9, 2005 Certification Standards for New Technologies Presentation to:
WILDFIRE UAS Concept of Operations US Forest Service Fire & Aviation Management DRAFT.
7-1 Design of UAV Systems Sorties ratesc 2002 LM Corporation Lesson objective - to discuss Sortie rate analysis including … - Mission planning and preparation.
Doris Hamill UAV Business Development Lead NASA Langley Research Center and Hampton Roads First Responders.
Can - SAT Project. Agenda Project Description CanSat Objectives Project Objectives Project Rules –Mandatory –Optional History of CanSAT Design Goals Team.
UK Aerial Robotics Team UK IDEA Laboratory Workforce Development: The UK Aerial Robotics Team and the PAX River Student UAV Competition Dale McClure (Matt.
Network UAV C3 Stage 1 Final Briefing Timothy X Brown University of Colorado at Boulder Interdisciplinary Telecommunications Program Electrical and Computer.
© Copyright 2008 Rockwell Collins, Inc. All rights reserved. Proprietary Information Rockwell Collins SAE ACGSC Meeting 102 General Committee Briefing.
DRONE: UNMANNED AERIAL VEHICLE Seminar Co-Ordinator:  Mr. A.K.Singh Seminar Presented by: Ajit Pal Singh.
Introduction to IWA. The IWA is based on a patented, next generation design called the Internal Wing Aircraft. The concept brings three separate wings.
Ship-based UAV Recovery System (SURS) Launch and Recovery of Manned and Unmanned Vehicles from Marine Platforms 2010 Symposium March 8-9, 2010.
THE TYPES OF TRANSPORT npor. Ing. Zuzana Sudolská.
FAA sUAS ARC Support Documentation © ASTM International. All Rights Reserved. The Unmanned Aircraft System Initiative F38 on Unmanned Aircraft Systems.
Logan Simon & Jackson Smith S&S Aeronautics. Problem Statement Drones are extremely useful in many applications including Aerial photography, Search and.
ES 100 Micro Air Vehicle Project Montgomery College Professor: Dr. Charles Kung Summer I 2012 Team Members: Andrew Joe Laura Mohammed Nathelie Noella Stephanie.
Mini Autonomous Flying Vehicle CASDE is part of the National effort to develop a Micro Air Vehicle. CASDE has chosen a Mini Vehicle, in the short term,
Minor Project on Vertical Take-off Landing System SUBMITTED BY:- SHUBHAM SHARMA ( ) ABHISHEK ARORA ( ) VIBHANSHU JAIN ( )
Unmanned Aerial Vehicles Plant and Weed Management Art Hirsch & Chris Rice January 7, 2015.
Mr. Lagomarsino Money Power with Technology Applications.
Frost & Sullivan Global Growth Partnership Services Aerospace & Defence Research Programme 2013.
DRAFT Strategic Customer Value Analysis May NAVAIR OVERVIEW INTERVIEW NAVAIR OVERVIEW INTERVIEW.
Unmanned Aircraft Systems
MGMT 203 Aeronautical Science, Aviation Professionalism, Careers, and Certification Module 1.
Helping Agriculture One Flight at a Time
MGMT 203 Aeronautical Science, Aviation Professionalism, Careers, and Certification Module 1.
MGMT 203 Aeronautical Science, Aviation Professionalism, Careers, and Certification Module 1.
PAX River Competition UK Aerial Robotics Team University of Kentucky.
UAV Vision Landing Motivation Data Gathered Research Plan Background
Unmanned Systems Aerospace Engineering
Unmanned Systems Aerospace Engineering
UA.I.A.K2.
Lockheed Martin Challenge
Overview of UAS World.
Brandon Maier, Project Manager
Unit 2 Unmanned Aircraft
Presentation transcript:

AT 209 Introduction to Civil Unmanned Aerial Systems (UAS) Professor M Leasure, Associate Professor AET (leasurem@purdue.edu) Class will meet 2 times per week for 50 minutes Includes both lecture presentation and hands-on use of UAV technology Airport hangars will be used for indoor flight operations Limited outdoor flight opportunities are available as needed Laboratory projects include simulator flight time and operation of various UAS platforms. A final group presentation will be required.

What you will learn in this class:   Demonstrate ability to manually fly unmanned aircraft visually and via remote video feed (FPV) Acquire basic skills related to unmanned aircraft operation with flight simulator technology Demonstrate ability to plan and execute mission plans for unmanned flights Acquire knowledge of unmanned aircraft, operating systems, and ground control options Demonstrate unmanned applications in achieving mission goals Propose unmanned aerial applications and develop implementation plan Present findings regarding proposed unmanned aircraft applications to class Acquire working vocabulary of unmanned flight descriptions Demonstrate autopilot installation, calibration, and system operation Demonstrate skills related to system construction and maintenance

Unmanned Aerial Systems-UAS This class will primarily focus on civil UAS applications and technology. Topics are as follows: 1. Introduction 2. History 3. Platform Options 4. Powerplant options 5. Airframe construction 6. Command and control systems (flight) 7. Launch and recovery options 8. Civilian applications 9. Regulations 10. Safety 11. Repair and maintenance 12. Sensor packages 13. Field Deployment Experience 14. Current assets and presentation Specifications

What is a UAS/UAV? The UAV is an acronym for Unmanned Aerial Vehicle, which is an aircraft with no pilot on board. UAVs can be remote controlled aircraft (e.g. flown by a pilot at a ground control station) or can fly autonomously based on pre-programmed flight plans or more complex dynamic automation systems. UAVs are currently used for a number of missions, including reconnaissance and attack roles. A UAV is defined as being capable of controlled, sustained level flight and powered by a jet, electric, or reciprocating engine. In addition, a cruise missile can be considered to be a UAV, but is treated separately on the basis that the vehicle is the weapon. The acronym UAV has been expanded in some cases to UAVS (Unmanned Aircraft Vehicle System). The FAA has adopted the acronym UAS (Unmanned Aircraft System) to reflect the fact that these complex systems include ground stations and other elements besides the actual air vehicles.

UAS Types by mission Target and decoy - providing ground and aerial gunnery a target that simulates an enemy aircraft or missile. (first used WW2) Reconnaissance - providing battlefield intelligence (most common) Combat - providing attack capability for high-risk missions (see Unmanned Combat Air Vehicle, (UCAV) Research and development - used to further develop technologies to be integrated into UAS aircraft Civil and Commercial UAVs - UAVs specifically designed for civil, and potential commercial, applications such as agriculture, forestry, etc.

Manual Flight Controls, Mode 2 FORWARD UP YAW LEFT ROLL RIGHT DOWN Back (up, down, right, left are referenced from virtual pilot seat)

UAS Sample Designs Lockheed Quadrotor

Another Lockheed design, small 5 pound Quadrotor

Viking Aerospace Helicopter 18 horsepower

Fixed Wing Large Civilian Ranger – Swiss/Israeli Civilian with catapult

Fixed Wing Small CALMAR Condor Agricultural Imaging UAV, 10’ span, 21 pounds loaded, Electric propulsion, hand launch, unimproved field landing

Flex Wing Wings can fold for storage

Powered parachute Very compact for transport, slow flight, low power required

Airship Power only used for climb and repositioning, vulnerable to high wind

VTOL Fixed Wing Vertical Take-off and landing combined with fixed wing speed

VTOL ( Tail Sitter) Fixed wing speed with no runway requirement

Components of a Complete UAS Operation COA application and approval of platform and flights (regulatory) Platform design and construction (manufacturing) Flight test and development (flight) Maintenance and repair of uas (technical) Training for all aspects (education) Coordinating and identifying applications with customers (marketing) Investigating new technology (research) Data package implementation, data analysis (data science) Onboard electronics, guidance, power, control (avionics) Coordination and monitoring of projects (management) Securing funding and income streams ( finance)  

END