Our project outlines development process of Y6 COAXIAL HIGH SPEED DRONE which consists of concept of motion, modeling of the vehicle dynamics, rapid prototyping of the mechanics and finally practical realization of the VTOL (A vertical take-off and landing aircraft)
PROJECT OBJECTIVE:
Our essential and most extreme goal was making a Y6 MULTIROTR HIGH SPEED DRONE which will be fit for maintaining the balance as well as flying at generally high velocity than other UAV'S.
SOCIO-ECONOMIC BENEFITS:
- Allow industries to realize savings from cost-effective means of inventory, transportation, and distribution.
- Easily Deployable
- Security.
- Privacy
- Filming Movies
- Delivering Packages
- Emergency Response
PROJECT METHODOLOGY:
Beginning with the edge, we took a HexaCopter frame and changed it in a manner to be utilized for Y shape (TRI COPTER), albeit lately we utilized the idea of multicolor to make it Y Shaped HexaCopter.
We utilized 1400KV brushless motors, 2 motors on one arm (coaxial) and abs propellers of 10" dia. Utilizing two motors for every arm implies one above and one beneath, bringing about their contrary developments like CW (clockwise) and CCW (Counterclockwise), so we utilized the propellers as needs be.
30 AMP ESC (electronic speed controllers) are utilized with each engine in equal association. Each ESC is independently aligned with point of view for motors. We didn't involved ESC'S in series on one arm to stay away from disappointments while flying since, supposing that they were associated and adjusted in series assuming one motor bombs the other one on a similar arm would likewise have been fizzled. To keep away from such disappointments we adjusted each ESC independently with separate motor so basically we can land securely if there should arise an occurrence of any disappointment. Every one of the alignments was done physically on Mission Planner.
3300 mah battery is utilized and APM 2.8 flight controller is utilized.
Recently we involved Ardupilot Y6B calibration as on one arm, one motor pivots CW and other turns CCW with the exception of the tail arm as it has inverse elements for motor revolutions and the upper motor pivots CCW while motor underneath the upper one is utilized for CW turn.
Our most memorable flight was in the college and it was an effective flight demonstrating that our UAV during the flight not just balanced itself which was a major test on multi rotors drone yet in addition achieved a High Speed.
PROJECT OUTCOME:
- Attained high speed.
- Complex design.
- Balancing at high speed.
- Affordable.
- First of its kind in Pakistan.
