Tilty was developed as a side research project during my first year as a Master's student. The main goal was to quickly develop a new tilt-rotor aircraft using off the shelf components and using a simple control system. This would enable us to quickly move from construction, to testing, without a lengthy code development time. It is important to remember this was built in 2017 before PX4 and Ardupilot had implemented tilt-rotor flight control. Once the aircraft was developed and transitioned, we examined different control schemes that could make the aircraft simpler for the test pilot. Two research papers were written about the project in depth and are linked at the bottom of the article.
The design takes off like a normal quadcopter and can use a standard quadcopter PID controller. In forward flight, the rear 2 rotors tilt backward to provide forward thrust while the front two rotors shut off. Control in airplane mode uses the same PID control loops used for the quadcopter controller with scheduled gains. In fact, the control surfaces are always reacting to the output from the PID in both hover and cruise. To quickly tune the system, the airplane gains and the quadcopter gains were tuned independently. During transition, the gains shift as the motors tilt. A full video of the transition is shown below. Despite the very simple control scheme, the design allows for a nice steady transition.
The paper below included in full, provides an in-depth summary of the design and construction process. The design was a collaboration between myself, my research adviser Dr. German, and undergraduate Frank Kozel. Thanks to Eddie Li for helping with the control code modifications. Undergraduates were mainly responsible for the construction while I was responsible for the propulsion, wiring, and flight control system. I also flew the airplane during all tests and managed the project.
The end result of the project was an airplane with steady characteristics in all phases of flight and with steady outbound and inbound transitions. We learned that the design of the tilt mechanisms is critical and that small asymmetries can cause instability especially during the inbound transition.
The final published research paper about the control system and testing is available here.
A preliminary paper focusing on the design and construction was written by one of the undergraduate researchers working with me on the project and was not published and is therefore available below.
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