R.C Air Plane

DESIGN AND FABRICATION OF RADIO CONTROLLED AIRPLANE sort Members ADEEL AHMAD(080304) BABUR MANSOOR(080316) BILAL IFTIKHAR(080319) HAFIZ FAIZAN SHABBIR USMANI(080332) BE MECHATRONICS (7-A) suggest supervisor Group Captain (R) Muzaffar Ali Assistant Professor DEPARTMENT OF MECHATRONICS ENGINEERING capacity OF ENGINEERING AIR UNIVERSITY, ISLAMABAD DESIGN AND FABRICATION OF RADIO CONTROLLED AIRPLANE Final Year Project Report (Fall) DEPARTMENT OF MECHATRONICS ENGINEERING DESIGN AND FABRICATION OF RADIO CONTROLLED AIRPLANE Submitted By ADEEL AHMAD(080304)BABUR MANSOOR(080316) BILAL IFTIKHAR(080319) HAFIZ FAIZAN SHABBIR USMANI(080332) Project Supervisor ____________________________ Assistant Professor, Group Captain (R) Muzaffar Ali Head of Department ____________________________ Professor/Dean/Chair Department, Engr. Dr. Zafar-ullah-Koreshi rascal IAcknowledgement. Page IITable of Contents Chapter 1 IntroductionPage no 02 1. 1 Basic IntroductionPage no(prenominal) 03 1. 2 Transmitter /ReceiverPage No. 04 1. 3 Microcontroller Page No. 05 1. 4 Digital GyroscopePage No. 05 Chapter 2 Literature Review Page No. 06 2. History Page No. 07 Chapter 3 Modeling & DesignPage No. 08 3. 1 Modeling of DC servo Motors Page No. 09 3. 2 Design of RC PlanePage No. 11 3. 3 Major Parts of RC PlanePage No. 12 3. 4 Mechanical AnalysisPage No. Chapter 4 ReferencesPage No. 14 4. 1 BooksPage No. 15 4. 2 WebsitesPage No. 15 Acknowledgements Apart from the efforts from us, the success of this project depends largely on the encouragement and guidelines of numerous others. We take this opportunity to express our gratitude to the people who have been instrumental in the successful completion of this project.We would the likes of to show our greatest appreciation to our project Supervisor Assistant Professor, Engr. Muzaffar Ali. We cant say thank you enough for his tremendous support and help. We feel motivated and encouraged every time we attend his meeting. Without his encouragement and g uidance this project would not have materialized. Need slight to mention that Sir Raheel Afzal & Sir Moeen Maboob, Lab Engineers, who had been a source of devotion and for their timely guidance in the conduct of our project work. We would also like to thank all the qualification Members for all their valuable assistance in the project work.Finally, yet importantly, We would like to express our heartfelt give thanks to our beloved p arents for their blessings, our friends/classmates for their help and wishes for the successful completion of this project. Chapter 1 Introduction 1. 1 Basic Introduction wireless Controlled (RC) plane is basically a smaller prototype of an actual aircraft and its dynamics are relatively c hallenging to understand. For RC Plane there is 3-degree of freedom. Important parameters are roll, pitch and yaw. To achieve control of these parameters, there are three control surfaces ailerons, elevators and rudder. 1. Transmitter/Receiver A Transmitter is an electronic device that generates and amplifies a carrier wave, modulates it with a meaningful point derived from speech or other sources, and radiates the resulting signal from an antenna. The transmitter used for project has 6 channels and is programmable for both airplanes and helicopters. It has a 3-way flap switch, aileron and elevator dual rate switches, rudder mix switch, gear and aux2 switch. A preset memory makes it possible to set up several different models on the same intercommunicate. AReceiverconverts signals from a radioantennato a usable form.It useselectronic filtersto separate a get byeradio frequencysignal from all other signals, theelectronic amplifier developments the level suitable for further processing, and ultimately recovers the desired information throughdemodulationanddecoding. Information carried on a radio signal may diddle sound, images or data. We are victimization a 6 channel tiny 4 grams receiver with signal path diversity. 1. 3 Microcontro ller We will be using Arduino AT-Mega 328 Microcontroller and it has a dedicated PWM pin. It has built in ADC thereof no external ADC is required and it is very much faster than Atmel Microcontrollers . 4 Digital Gyroscope How Gyroscopes counterfeit Gyroscope can balance on almost on any surface with single strive It can be a finger or even a string. They can resist dubiousness about the spin axis in very odd ways but the most provoke effect is that gravity-defying part which is calledPrecession. We will be using Eclectic Gyroscope in our RC Plane to show it with stable Flight. We are using Gyro ITG 3200. Chapter 2 Literature Review 2. 1 History The earliest examples of electronically guided model aircraft were hydrogen-filled modelairshipsof the late 19th century.They were flown as a music hall act around theater auditoriums using a basic form of spark-emitted radio signal. In 1920s, the kingly Aircraft Establishmentof Britain built and tested the Larynx, amonoplanewith a degree centigrade-mile (160km) range powered by a lynx engine. It was not until the 1930s that the British came up with the Queen Bee, a modifiedde Havilland Tiger Moth, and similar train aircraft. Radio control technology has been in use since 1893, when Nikola Tesla created a boat that was controlled by transmitted radio waves. In 1917, the first radio controlled airplane was successful.During World War II, Germany tried a variety of weapons that were operated by radio control. Radio controlled model airplanes have evolved over the years and seen improvements since that first flight in 1917. Chapter 3 Modeling & Design 3. 1 Modeling of DC Servo Motrors 3. 2 Design of RC Plane 3. 3 Major Parts Of RC Plane Rudder Flex the rudder back and forth to loosen up the foam hinge. The less force needed to move the rudder the less stress is put on the servo during flight. Alternatively cut them off and use clear packing tape to re-attach them, one slice on each side. pic ElevatorAdjust the plump adjust value to the maximum allowed before the servo begins to bind. pic Wings Helps the Plane in gliding and to increase the surface area of the plane. pic Aileron For maximum throw, the aileron wing servo has to be swapped around vertically. The servo head should be pointing toward the back instead of the leading wing edge 4. Mechanical Analysis All dimensions of the Plane are From National Advisory Committee for Aeronautics(NACA) , we selected the NACA series of 0015 as it was cheaper to fabricate. The Analysis of the Aerofoil was performed on gambit & Fluent as these software are used for fluid analysis.We calculated the Coefficient of Drag & Lift using these software to determine whether the plane will fly or not. The coordinates of the NACA series 0015 was taken from the NACA site. Theoretical Calculations space of Aerofoil (chord)= 19 cm Max Thickness of Aerofoil=2. 85 cm (2. 85/19)*100= 15 We Know that our Aerofoil is Symmetrical, therefore the The NACA Series num ber of our Foil is 0015 The NACA 0015 airfoil is symmetrical, the 00 indicating that it has no camber. The 15 indicates that the airfoil has a 15% compendiousness to chord length ratio it is 15% as thick as it is long.NACA 0015 1. 000000, 0. 001580 0. 950000, 0. 010080 0. 900000, 0. 018100 0. 800000, 0. 032790 0. 700000, 0. 045800 0. 600000, 0. 057040 0. 500000, 0. 066170 0. 400000, 0. 072540 0. 300000, 0. 075020 0. 250000, 0. 074270 0. 200000, 0. 071720 0. 150000, 0. 066820 0. 100000, 0. 058530 0. 075000, 0. 052500 0. 050000, 0. 044430 0. 025000, 0. 032680 0. 012500, 0. 023670 0. 000000, 0. 000000 0. 012500, -0. 023670 0. 025000, -0. 032680 0. 050000, -0. 044430 0. 075000, -0. 052500 0. 100000, -0. 058530 0. 150000, -0. 066820 0. 200000, -0. 071720 . 250000, -0. 074270 0. 300000, -0. 075020 0. 400000, -0. 072540 0. 500000, -0. 066170 0. 600000, -0. 057040 0. 700000, -0. 045800 0. 800000, -0. 032790 0. 900000, -0. 018100 0. 950000, -0. 010080 1. 000000, -0. 001580 Chapter 4 Refer ences 6. 1 Reference Books 6. 2 References Web-Sites file///G/GBx%20Brushless%20Motor%20Calculator. htm http//www. futaba-rc. com/ http//www. mathworks. com/products/sl-design-optimization/demos. html? file=/products/demos/ merchant marine/sldo/spe_servomotor. html http//www. futaba-rc. com/servos/brushless. html www. 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