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Oct 30, 2020
FINAL YEAR PROJECT SYNOPSIS 3-D MAPPING AUTONOMOUS FLIGHT QUADCOPTER WITH
INDUCTIVE CHARGING
Submitted by:
Muhammad Ayaz Qureshi 2013-EE-27
Muhammad Ismail Saleem 2013-EE-29
Wajid Ali 2013-EE-35
Hummad Ahmed Usmani 2013-EE-46
Supervised by: Dr. Khalid Mahmood ul Hassan
Department of Electrical Engineering
University of Engineering and Technology Lahore
FINAL YEAR PROJECT SYNOPSIS 3-D MAPPING AUTONOMOUS FLIGHT QUADCOPTER WITH
INDUCTIVE CHARGING
Submitted to the faculty of the Electrical Engineering Department
of the University of Engineering and Technology Lahore
in partial fulfillment of the requirements for the Degree of
Bachelor of Science
in
Electrical Engineering.
Final Year Project Advisor Final Year Project Coordinator
Department of Electrical Engineering
University of Engineering and Technology Lahore
i
Declaration
I declare that the work contained in this synopsis is my own, except where explicitly
stated otherwise. In addition this work has not been submitted to obtain another degree
or professional qualification.
Signed:
Date:
ii
Acknowledgments
We express our deep sense of gratitude to Professor Dr. Khalid Mahmood ul Hassan,
for accepting our final year project proposal. May Almighty Allah gives us health and
ability to complete this project sucessfully.
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To our parents, teachers and all the well wishers out there . . .
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Contents
Acknowledgments iii
Abbreviations vii
Abstract viii
1 Introduction 1
2 History 2
2.1 Recent Developments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2
3 Objectives 4
3.1 Automation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4
3.2 Wireless Charging . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4
3.3 Wireless Communication . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4
3.4 Self-Balanced System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4
3.5 3-D Mapping . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5
3.6 Techniques to Implement 3-D Mapping . . . . . . . . . . . . . . . . . . . . 5
4 Rough Cost Analysis 6
5 Software Tools 7
6 Project Feasibility 8
7 Estimated Completion Time and Flow Chart 9
7.1 Deliverable . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9
7.2 Project Flow Diagram . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10
8 Prospective Problems 11
9 Future Work and Applications 12
9.1 Future Work . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12
9.2 Applications . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12
10 Block Diagram 13
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Contents vi
References 15
Abbreviations
UAVs Unmanned Aerial Vehicles
GUI Graphical User Interface
SFM Structure From Motion
ESC Electronic Speed Control
PMA Powermat compatible standard
Qi Wireless Power Consortium standard
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Abstract
Quad-Copter is an Unmanned Aerial Vehicle (UAV) which is operated to fly indepen-
dently. In our project, we are designing a fully automated Quad-Copter programmed
in a manner, that will fly a specific amount of distance for specific period of time and
then it will sense its landing pad and will land there. Quad copter will move and hover
around by keeping its stability maintained. The conventional quad copters requires a
continuous charging of quad copters but in this project we are including wireless charg-
ing system also named as inductive charging. In addition to automation we are boosting
it up with wireless communication system. So in wireless communication Quad-Copter
can be controlled manually by using a graphical user interface, giving full control to the
user. Conventional Quad-Copters are provided with 2-D mapping capability but our
project surpass their 2-Ds map because we are introducing 3 D map in which concept
of rasterization and image processing is employed. After landing image processing soft-
ware will stitch these photos into 3-D map. So our automated Quad-Copter is capable
of taking the flight after some specified interval of time, collecting all the possible data
regarding 3D-layout (digitized sketch) of any section, and on returning back to its pad,
Quad-Copter send this sketch to working unit on GUI interface.
Chapter 1
Introduction
With the advancement in engineering and technology, there was a dire need of an in-
troduction of device which can go to places where humans cannot, which will enable
them to do much. Also there was a need of device which help take human in the air
in a very much fascinating way. A device was needed which can capture aerial images.
These devices which have revolutionized the flight are called as drones and quad-copter.
The way in which these devices are developed through decades is fascinating. Drones
belongs to a class of air vehicles known as Unmanned Aerial Vehicles (UAVs). These
vehicles can take off in the air without pilots. Drones are basically flying robots. They
have software control integrated in their environment.
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Chapter 2
History
The quad-copter designs have been around for a very long time, but the design is inher-
ently unstable. With 4 rotors spinning, keep them moving at the right speed to keep the
quad-copter level and stable is difficult. In November of 1922, Etienne first flew improved
helicopter featuring vertically mounted rotors which rotated in the opposite direction
from the large top rotors. Quad-copters today still use this same basic design. The
Convertawings Model A quad-copter designed by Doctor George E Bothezat appeared
in 1956. It was the first to use propulsion, or a propellers forward thrust to control an
aircrafts roll, pitch and yaw. Recent advances in technology have addressed issues that
plagued early quad-copter design, including poor stability, limited control and complex-
ity. Modern quad-copters are very stable, easy to control and easy to fly. At a small size,
quad-copters are cheaper and more durable than conventional helicopters due to their
mechanical simplicity. Their smaller blades are also advantageous because they possess
less kinetic energy, reducing their ability to cause damage. For small-scale quad-copters,
this makes the vehicles safer for close interaction. Increasing blade size improves effi-
ciency as it takes less energy to generate thrust by moving a large mass of air at a slow
speed than by moving a small mass of air at high speed but it takes at the cost of control.
2.1 Recent Developments
In the last few decades, unmanned aerial vehicles including quad-copters have been used
for many applications. The need for aircraft with greater hovering ability has led to a
rise in quad-copter research. The four-rotor design allows quad-copters to be relatively
simple in design yet highly reliable. Research is continuing to increase the abilities
of quad-copters by making advances in multi-craft communication, environment explo-
ration. If these developing qualities can be combined, quad-copters would be capable of
advanced autonomous missions that are currently not possible with other vehicles.
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Chapter 2. 3
Some current programs include:
• Bell Boeing Quad Tilt Rotor : concept takes the fixed quad-copter concept further by combining it with the tilt rotor concept.
• Parrot A.R.Drone : is a small radio controlled quad-copter with cameras at- tached to it, designed to be controllable by smartphones or tablet devices.
• Nixie : is a small camera-equipped drone that can be worn as a wrist band.
As far as recent development regarding inductive charging is concerned it is being em-
ployed in mobile industry and electric vehicles. In 2015 Samsung announced the new
S6 and S6 Edge with wireless inductive charging through both Qi and PMA compatible
chargers. Blackberry also released phone to support wireless inductive charging through
compatible chargers. In electric vehicles in one inductive charging system, one winding
is attached to the underside of the car, and the other stays on the floor of the garage.
While as far as 3 D mapping is concerned, in industry and in many applications there
is a dire need of a system which can rapidly, reliably, remotely and accurately perform
measurements in three-dimensional space for the mapping of environment. From now
onwards there will be a lot of research on 3 D mapping. Previous work comprises of
invention seeks to provide a method of locating at least a surface and modeling the
surface using at least two image capture. A considerable amount of work has been done
by researchers in the field of machine vision and image analysis.
Chapter 3
Objectives
3.1 Automation
Designing a fully