AJMAN UNIVERSITY OF SCIENCE & TECHNOLOGY
COLLEGE OF ENGINEERING
DEPARTMENT OF ELECTRICAL ENGINEERING
Supervised by:
Dr. Samir Tozin
Prepared by:
Faezah Gholam 200910879
Sama kutaiba 201011183
Rawan Jamal 200910880
Safa alghadi 201011935
• To successfully implement a working prototype of automated synchronized quad-copter flight.
• To design Quadcopter that can control wireless base on computer.
• To stabilize quad-copter based on integrated gyroscope and accelerometer.
• Develop quad-copter that would have the capability of indoor flight.
• Hold quad-copter at certain altitude and following a track.
Quadcopter main axises :
Pitch , yaw and roll.
motions of quadcopter:
- Take-off and landing motion mechanism.
- Forward and backward motion.
- Left and right motion
Quadcopter
Future plan
- Controlling quadcopter through PC .
- Hovering quadcopter at certain altitude.
- Quadcopter flying over a track
What is Quadcopter
components for the control board
Quadcopter flying mechanism
Quadcopter (quadrotor helicopter) is a multicopter that is lifted and propelled by four rotors
- Arduino Uno
- 3-IR sensors
- Ultrasonic sensor
- IMU sensor
- ESC
- XBee
Thanks for listening
Conclusion
System's block diagram
The main objectives
Why we call it autonomous
- To protect the quadcopter from crashing into obstacles we will add sensor to the design .
- It needs a lot of tests and implementation before writing the code for each part and in each time we add extra sensor or any other component.
- The most challenging part of the project will be to make the quadcopter hover in a fixed position without drifting.
quadcopters fly without need to any help or instruction.