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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.

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