Deliverable 3 Autonomous Flight Record

Similar documents
Design and Development of the UTSA Unmanned Aerial System ACE 1

SURVEYOR-H. Technical Data. Max speed 120 km/h. Engine power 7.2 hp. Powerplant Modified Zenoah G29E. Fuel tank volume 3.6 l

Length Height Rotor Diameter Tail Rotor Diameter..12. Tail Boom Length Width

DSSI UAV. Unmanned Aerial Vehicle. Research & Development Project

PENGUIN B UAV PLATFORM

Electric Penguin s philosophy:

Palos Verdes High School 1

UAV KF-1 helicopter. CopterCam UAV KF-1 helicopter specification

BY HOEYCOMB AEROSPACE TECHNOLOGIES. HC-330 HYBRID-POWERED ALL- ELECTRICITY DRIVEN four-rotor UAV

2015 AUVSI UAS Competition Journal Paper

ROBUST AIRFRAME FOR UAV FLIGHT TESTING FOR SALE!

Overview. Mission Overview Payload and Subsystems Rocket and Subsystems Management

Deliverable 2: Technical Report

DRONE & UAV.

Investigative Technologies and Techniques

Speedy F250-V2. Naze-6DOF. Quick Start Guide

In 2003, A-Level Aerosystems (ZALA AERO) was founded by current company President Alexander Zakharov, since then he has led

AERO. Meet the Aero. Congratulations on your purchase of an Aero!

Technical Journal Paper

Massachusetts Institute of Technology Unmanned Aerial Vehicle Team. Jonathan Downey, Derrick Tan. June 16, Abstract

THE FALCON REDUNDANCY HIGH WIND TOLERANCE BEST USED FOR SURVEILLANCE & SECURITY DELIVERY & TRANSPORT

SRM-UAV AUVSI SUAS 2015 JOURNAL PAPER

Warning! Before continuing further, please ensure that you have NOT mounted the propellers on the MultiRotor.

AT-10 Electric/HF Hybrid VTOL UAS

Unmanned Aerial Vehicle Design, Development, and Implementation

MAVIC 2 PRO. Quick Start Guide V1.2

Development of an Autonomous Aerial Reconnaissance Platform at Virginia Tech

2012 AUVSI SUAS Student Competition Journal Paper. Kansas State University Salina UAS Club. Prepared By: Mark Wilson Coby Tenpenny Colby Walter

Sabino Canyon UAV. text; Electronic Thesis. Pineda, Stephen Michael Joseph. The University of Arizona.

Development of a Low Cost DIY UAV Mapping Platform

AERO. Meet the Aero. Congratulations on your purchase of an Aero!

Aircraft 1. Gimbal and Camera 9. Link Button 2. Downward Vision System

AUVSI SUAS 2013 Journal Paper

Autopilot and Ground Control Station for UAV

Answer Key. Page 1 of 10

TABLE OF CONTENTS. Thank you for your interest in CUAir

FLYEYE Unmanned Aerial System

AUVSI Student Competition 2014 Journal Paper

North American F-86F Sabre USER MANUAL. Virtavia F-86F Sabre DTG Steam Edition Manual Version 1

Super Squadron technical paper for. International Aerial Robotics Competition Team Reconnaissance. C. Aasish (M.

MAVIC AIR. Quick Start Guide V1.2

Maryland UAS Team. Fall

Autopilot and Ground Control Station for UAV

The Doomerang University of California, Los Angeles

Ejemplos de aeronaves existentes similares a las propuestas en los RFP 2007

The drones are coming!

YS-X4 Multirotor Flight Controller-Hobby

Appenidix E: Freewing MAE UAV analysis

PENGUIN C UAS OPERATIONS & MAINTENANCE TRAINING 20 HOURS FLIGHT ENDURANCE 100KM RANGE ITAR - FREE CREW OF TWO

Flint Hill School Animus Ferus 2016 AUVSI SUAS Journal Paper. Abstract. Flint Hill School - Animus Ferus 1

WingtraOne Technical Specifications

Designed In The Future

Helicopter Experience, Date: August 1-6 Location: Central Connecticut State University

A complete hybrid VTOL autopilot solution. Start anywhere, fly everywhere.

Maryland UAS Team AUVSI SUAS Competition Journal Paper

Autonomous payload drop system using mini Unmanned Aerial Vehicles

Development and Testing of the X-2C Unmanned Aircraft System for the 2009 AUVSI Student UAS Competition

QUAD. Unfold arms and legs

Challenges of Rotary Aircraft Rotating Component Instrumentation

Lockheed Martin Corporation

CESSNA 182 CHECKLIST. LEFT WING Trailing Edge 1. Aileron CHECK freedom of movement and security


GACE Flying Club Aircraft Review Test 2018 N5312S & N5928E. Name: GACE #: Score: Checked by: CFI #:


DESIGN AND FABRICATION OF AN AUTONOMOUS SURVEILLANCE HEXACOPTER

KCN AREO CLUB CESSNA 152 ABBREVIATED CHECKLIST

Brief introduction

Best Glide 75 kias (Max Gross)

DemoSat-B User s Guide

The Institution of Engineering and Technology Seminar on. Micro UAVs. Dr Tom Richardson University of Bristol. 20 th February 2007

Bild : Bernhard Mühr German Aerospace Center Flight Operations

Operation Manual. IMPORTANT Read before flying!

CESSNA 172N 08E/97E CESSNA 172N 08E/97E PREFLIGHT INSPECTION

Y. Lemmens, T. Benoit, J. de Boer, T. Olbrechts LMS, A Siemens Business. Real-time Mechanism and System Simulation To Support Flight Simulators

LAGARI 2017 Technical Design Paper for AUVSI Student UAS Competition

Presentation Outline. # Title # Title

Checklist LN-DAG SFK 2014

TECNAM P2004 BRAVO N128LS

DOBBY Pocket Drone. Quick Start Guide V2.1

G4 RECON ONE Product overview and performance features

Development, Certification, and Flight Testing of an OPA for UAS FTT Development and Training at NTPS

University of Alberta Aerial Robotics Group Unmanned Aerial System

Texas A&M UAV Design Texas Buzzard

Mississippi State University Team X-ipiter X AUVSI Undergraduate Student UAS Design Competition

Polytechnic University s Unmanned Aerial Vehicle Design. Journal Paper AUVSI Undergrad Competition

In response to. 34th Annual AHS International Student Design Competition IIT KANPUR INDIAN INSTITUTE OF TECHNOLOGY, KANPUR

A B C D E F G H J K L M N

V - Speeds. RV-10 V fe Flaps Speeds Trail (0 deg) Half (15 deg) Full (30 deg) 122 kias 96 kias. 80 kias

FPV MICRO DRONE Indoor / Outdoor Wireless Quadrocopter ATOM INSTRUCTION BOOKLET. Trim size 4.5 x in. Spread size 9 x in.

Fire Fighting Equipment Development - Unmanned Aerial Vehicle Trials. Ripley Valley Rural Fire Brigade - August 2010

AEROCARDS CALVERT HALL COLLEGE HIGH SCHOOL 2015 JOURNAL

TECNAM P92 EAGLET N615TA TECNAM P92 EAGLET CHECKLIST [FLIGHT PLAN DESIGNATION IS ECHO ]

JODEL D.112 INFORMATION MANUAL C-FVOF

CHECKLIST N8876B Cessna 172. Nebraska Flight Center Eppley Airfield 3737 Orville Plaza Omaha, NE Tel. (402)

Electric VTOL Aircraft

CESSNA 172I CESSNA 172I PREFLIGHT INSPECTION

OPERATIONS MANUAL FTO SECTION : 06.04

1 Closed Loop Speed Control (Fixed Wing) This manual is an addendum to the Vector and MicroVector manuals.

Table of Contents. Abstract... Pg. (2) Project Description... Pg. (2) Design and Performance... Pg. (3) OOM Block Diagram Figure 1... Pg.

Eurathlon Scenario Application Paper (SAP) Review Sheet

Transcription:

Deliverable 3 Autonomous Flight Record 2012 UAV Outback Challenge Search and Rescue Challenge www.canberrauav.com Proudly Sponsored by: Paul Tridgell Terry Porter Grant Morphett Ron Graham Page 1 of 11

1 Table of Contents 1 Table of Contents... 2 2 Flight Logs... 3 2.1 Flight Log Book... 3 2.2 GPS Telemetry... 5 2.3 Video... 5 2.4 Static Images... 5 3 RF Transmitters... 10 3.1 2.4 GHz RC Link... 10 3.2 900 MHz Telemetry Link... 10 3.3 5.8 GHz Image and Telemetry Link... 10 4 Aircraft Specifications and Performance... 11 Page 2 of 11

2 Flight Logs 2.1 Flight Log Book The following is an extract from our flight log book. Date Aircraft Start Flight AUTO Flight Comments Bottle Drop? Camera capturing? Time Time time 06/01/12 Mugin 1030 4:52 0:00 Recording flight characteristics in order to tune autopilot. Not fitted Not fitted 05/02/12 Mugin 1039 8:14 0:00 Tuning of the autopilot s stabilisation parameters. Not fitted Not fitted 22/04/12 Mugin 1114 10:00 0:00 Testing telemetry streams and bottle drop mechanism. Also capturing Bottle released. Not fitted video for Deliverable 2 Parachute did not open 01/07/12 Mugin 1105 38:18 35:40 Failsafe module (V1) test OK. Rough landing slight nosewheel damage needs fixing. Dead stick landing Suspect engine tuning problem. Excellent waypoint tracking. Not fitted Not running 07/07/12 Mugin 1114 44:18 41:03 Onboard computer crashed during flight. Motor stopped during flight. Dead stick landing. Some damage to nosecone Not fitted 16700 images captured. Joe successfully found by shirt colour 07/07/12 Mugin 1342 36:47 34:51 Motor stopped during flight. Dead stick landing. Not fitted 23320 images captured. Joe found by shirt colour 15/07/12 Mugin 1301 36:05 34:40 Very high winds. Mugin coped exceptionally well. 5.8 GHz radio link unreliable, possibly due to depleted avionics battery. 15/07/12 Mugin 1433 19:00 12:07 Testing fuel system only filled tank to 1/3 to determine fuel cutout problem. Engine cut-out. Dead stick landing. HSV image filter tested. 21/07/12 Mugin 1239 68:49 62:11 New header tank fitted. Airspeed sensor more accurate. Main wheel strut showing signs of delamination. Not fitted Not fitted Unsuccessful. Bottle did not release 9069 images captured. Joe found by shirt colour No images captured Camera connection problem. 29357 images captured. Joe recognised successfully Page 3 of 11

Date Aircraft Start Flight AUTO Flight Comments Bottle Drop? Camera capturing? Time Time time 29/07/12 Mugin 1340 54:48 45:29 Replaced bung on header tank. Possible elevator issue causing difficulty maintaining consistent altitude. Image scoring functioning well Successful 25752 images captured. Joe successfully found 04/08/12 Mugin 1155 63:55 58:12 Very high wind gusting over 25 knots with significant cross component. Auto flight successfully coped with wind. Tested new blue filtering algorithm on image detection. Successful 26341 images captured. Joe successfully found Total 6:25:06 5:19:06 Page 4 of 11

2.2 GPS Telemetry A KML log of the first 35 minutes of the flight from 21/07/12 is shown below: The full file is available from https://docs.google.com/open?id=0bxjbg_6ksz5ztmo4ne5xdm1yumm. The file is in kmz format and is able to be opened in Google Earth. 2.3 Video A video showing the aircraft during autonomous flight and the operational ground station is available at http://youtu.be/8ofaq-7ko3y. 2.4 Static Images The following are a set of static images showing the ground station, aircraft and team members during flight operations from a number of flights over the last 3 months. Pre-flight checks Page 5 of 11

Pre-flight checks Fuelling the UAV before flight Starting the engine Page 6 of 11

Taxiing to the runway for takeoff Starting the takeoff run Takeoff Page 7 of 11

The Ground Station during flight. The Ground Station during flight. Page 8 of 11

During automated flight Removing the UAV from the runway after landing Page 9 of 11

3 RF Transmitters 3.1 2.4 GHz RC Link This link is used for manual RC control of the UAV s throttle and flight control surfaces. Specification Model Transmission Frequency Transmitter Power Transmitter antenna gain Calculated EIRP Covering licence Value FrSky DJT 2.4 GHZ 2400 2483.5 MHz 60 mw (17 dbm) < 5 dbi < 23 dbm Radiocommunications (Low Interference Potential Devices) Class Licence 2000. Part 45A, 53, 54 C-tick No. N14939 3.2 900 MHz Telemetry Link This is a low bandwidth link for transmitting telemetry from the UAV to Ground Station. Commands can be sent from the Ground Station to UAV when necessary. They have been calibrated and tested for LIPD-2000 (Part 52) compliance by RFDesigns RF lab in Brisbane. Specification Model Transmission Frequency Transmitter Power Transmitter antenna gain Calculated EIRP Covering licence Value RFD900 Telemetry Radio 915 928 MHz, 50 Channel Hopping 27 dbm 3 dbi 30 dbm Radiocommunications (Low Interference Potential Devices) Class Licence 2000. Part 52 3.3 5.8 GHz Image and Telemetry Link This is a high bandwidth link for transmitting images from the UAV s on-board cameras to the Ground Station. As a backup, the telemetry and command datastream also uses this link. Specification Model Transmission Frequency Transmitter Power Transmitter antenna gain Calculated EIRP Covering licence Value Ubiquiti Bullet M5HP 5750 MHz 25 dbm (UAV) 16 dbm (Ground) 5 dbi (UAV) 20 dbi (Ground) 30 dbm (UAV) 36 dbi (Ground) Radiocommunications (Low Interference Potential Devices) Class Licence 2000. Part 45B, 55 C-tick No. N14691 Page 10 of 11

4 Aircraft Specifications and Performance The Aircraft platform used by Canberra UAV is a Mugin (donated by CyberTechnology P/L). It has the following specifications: Specification Maximum Airspeed Cruise Airspeed Endurance at maximum airspeed Endurance at cruise airspeed Maximum take off weight Competition take off weight Wingspan Airframe length Identifying marks Aircraft planform and configuration Value 100 kts (180 Km/h) 50 kts (90 Km/h) Estimated 30 minutes 80 minutes 22 Kg 18 Kg 3 m 2.5 m 08WA on side of fuselage Twin boom V-tail pusher aircraft Page 11 of 11