This paper aims to present a comparison between different controllers to be used in a dynamic model of a quadcopter platform. The controllers assumed in this work are an ITAE tuned PID, a classic LQR controller and a PID tuned with a LQR loop. The results were obtained through simulations for 10 different attitudes of the quadcopter, however, in this paper simulation results will be presented for the vertical attitude only (the remainder are analogous and were omitted for brevity).
|Title of host publication||2013 International Conference on Informatics, Electronics and Vision (ICIEV)|
|Publisher||Institute of Electrical and Electronics Engineers Inc.|
|Publication status||Published - 1 Aug 2013|
|Event||2013 2nd International Conference on Informatics, Electronics and Vision, ICIEV 2013 - Dhaka, Bangladesh|
Duration: 17 May 2013 → 18 May 2013
|Conference||2013 2nd International Conference on Informatics, Electronics and Vision, ICIEV 2013|
|Period||17/05/13 → 18/05/13|