The project is about design of an Autonomous Hexcopter. This project will be a prototype for small autonomous aerial delivery vehicle. The drone will use Global positioning system based tracking and localization system and to automatically locate destinations. Main controller will send Global positi
Falcon Dot D Autonomous Delivery Hexacopter
The project is about design of an Autonomous Hexcopter. This project will be a prototype for small autonomous aerial delivery vehicle. The drone will use Global positioning system based tracking and localization system and to automatically locate destinations. Main controller will send Global positioning system coordinate back to the ground station using global system for mobile communication module where its position will be displayed on a Google maps. Main controller will also control pitch, yaw and roll based upon the gyro and accelerometer sensors values. Proportional-Integral-Derivative (PID) algorithm will use for the stability of the drone during flight. The drone would able to carry payload via using a servo gripper which is being controlled by main controller. When hexacopter reaches its destination it will drop the payload using gripper and come back to its starting position. Applications of this project are delivery of medicine, fast food, goods and important documents in the remote areas.
Objectives of this project is describe below
Overall implementation of design is described below:

Flight Controller
A flight controller for drone is usually an integrated circuit made up of microcontroller, sensors, and input/output pins. The simple job of the flight controller is to control the power and RPM of each motor by using the information received from sensors. Flight controller does not know already which type of your drone configuration and specification. So you need to set the specification and type of drone in the software program. Then upload the program in the flight controller. Gyro measures the rate of angular change up to three angular axes. Units of gyro are usually in degree per second. The output of gyro is usually analogue or I2c. You don’t need to worry about the output of the gyro since it is handled by the flight controller code. The gyroscope should be mounted so that its rotational axes line up with the axes of the drone Accelerometer measure the liner acceleration of the drone in up to three axes. Units of the accelerometer are in gravity which is 9.81 meter per second per second. The main characteristic of accelerometer is that they detect gravity with help of this as such can know which direction is down. So, it played very important role in the stability of the drone. The accelerometer should be mounted to the flight controller so that the linear axes line up with the main axes of the drone. Embedded Controller The Embedded controller or main controller is the brain of our drone. Flight controller algorithm is also run in the embedded controller. All the sensors are interface with our embedded controller. Sensors give values to our embedded controller. And then embedded controller control motors according to the flight controller algorithm i.e., PID. Design of hexacopter ESC (Electronic speed control) are devices that allow flight controller to adjust the speed of motors. Since design of drone is hexacopter so six ESC and six b 360kv motors are used in this project. Motors require 22 volts so 6s lipo batteries are used in the project. Tracking Mechanism For tracking drone live location usually GPS (Global Positioning System) is used. GPS use signal send by different satellites around the orbit to determine the specific geographic location. Flight controller have external or on board GPS mounted on them. GPS send coordinates to embedded system then these coordinates send to ground station using different wireless module. On ground station different software used to see these coordinates visually on Google maps.
Main benefits of the project are
These are the final deliverable of the project
| Flight time (minutes) | Payload (kg) |
| 31 | 1 |
| 15 | 2 |
| 10 | 3 |
| 7 | 4 |
| 6 | 5 |
Flight time (minutes)
31
15
10
7
6
| Elapsed time in (days or weeks or month or quarter) since start of the project | Milestone | Deliverable |
|---|---|---|
| Month 1 | PID and Hexacopter Theory study | Literature review document |
| Month 2 | Assembly of frame motors esc and flight controller | Hexacopter Model |
| Month 3 | Interfacing of GPS with Pixhawk | GPS coordinates shown on Mission Planner Software |
| Month 4 | Interfacing motors esc with Pixhawk, And remote. | Working Model of Hexacopter |
| Month 5 | Interfacing servo gripper | Payload will be grip and release |
| Month 6 | Testing and debugging | Final Hexacopter Prototype |
| Month 7 | Final working and documentation | Integration of different project parts and documentation |
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