A NOVEL FLIGHT CONTROLLER DESIGN FOR MODULAR APPLICATIONS

Authors

  • Marc Francis Say Department of Electronics and Computer Engineering, Gokongwei College of Engineering, De La Salle University, Manila, Philippines
  • Alvin Chua Department of Mechanical Engineering, Gokongwei College of Engineering, De La Salle University, Manila, Philippines
  • Edwin Sybingco Department of Electronics and Computer Engineering, Gokongwei College of Engineering, De La Salle University, Manila, Philippines
  • Maria Antonette Roque Department of Electronics and Computer Engineering, Gokongwei College of Engineering, De La Salle University, Manila, Philippines
  • Leonard Ambata Department of Electronics and Computer Engineering, Gokongwei College of Engineering, De La Salle University, Manila, Philippines
  • John Amos Tan Department of Electronics and Computer Engineering, Gokongwei College of Engineering, De La Salle University, Manila, Philippines
  • Clarisse Crespo Department of Electronics and Computer Engineering, Gokongwei College of Engineering, De La Salle University, Manila, Philippines
  • Reginald Rivera Department of Electronics and Computer Engineering, Gokongwei College of Engineering, De La Salle University, Manila, Philippines
  • Jayson Piquero Department of Electronics and Computer Engineering, Gokongwei College of Engineering, De La Salle University, Manila, Philippines

DOI:

https://doi.org/10.11113/aej.v12.17561

Keywords:

Casing, Flight controller, Pixhawk, Pixhawk cube, UAV

Abstract

A local flight controller was developed for modular applications based on the Pixhawk 1 flight controller with modifications to accommodate companion computer provision for future integration. This design is made for future modular applications, but for now, the functionality and performance of the local flight controller were tested and compared to the Pixhawk flight controller. A simple 3D printed enclosure was made to house the local flight controller for easier mounting on UAV frames. To compare the performance of the developed controller, two setups were made:  local flight controller and Pixhawk 1 on separate quadcopter frames, and local flight controller and Pixhawk Cube on separate fixed-wing frames. The flight controllers made use of the Ardupilot firmware, specifically ArduCopter and ArduPlane in conducting the flight tests. Auto flight mode was used to have autonomous flights which were then used to compare the flight data between test setups. The desired position and actual position were compared for each flight controller, and their differences with the other flight controllers were compared to see the variation between the different controllers used. After analyzing the data, the local flight controller developed was proven able to produce comparable results with the Pixhawk flight controllers. The percent difference between the mean values of the Pixhawk 1 and the local flight controller were 3.7064% and 8.6128% using the quadcopter frame for Position X and Y, respectively, while for the Pixhawk Cube and the local flight controller, the values were 12.6866% and 1.1045% using the fixed-wing frame, respectively.

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Published

2022-11-29

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Articles

How to Cite

A NOVEL FLIGHT CONTROLLER DESIGN FOR MODULAR APPLICATIONS. (2022). ASEAN Engineering Journal, 12(4), 151-155. https://doi.org/10.11113/aej.v12.17561