Oktaf Agni Dhewa, Faisal Fajri Rahani
The quadrotor's ability to maintain position is a major requirement for the completion of various current missions. However, the large steady-state error (SSE) and multiple overshoots due to environmental disturbances cause flight instability. This condition makes Quadrotor unable to complete the mission optimally. Therefore, in this study applying a linear quadratic regulator control method, this research contributes to the addition of integrator compensation in handling the translational movement of the quadrotor. System model design testing is carried out by comparing quadrotor control using the LQR method without an Integrator and LQR with an Integrator. The value of R=1 for all states and Q_x=0.87, Q_y=124.6, Q_(v_x)=1.77, Q_(v_y)=124.6 and Ki_x=0,004, Ki_y=0.002 makes the SSE tendency that occurs 0.10 meters for the x-axis and-0.28 for the y-axis, while the multi-overshoot that occurs is 0.41 m for the maximum deviation and-1.35 m for the minimum deviation on the x-axis and 0.40 m maximum deviation and 0.47 m minimum deviations on the y axis. The test results show that the LQR control method with Integrator compensation is able to minimize and improve SSE and multiple overshoots that occur in quadrotor flights. In addition, it is able to significantly increase accuracy to 100% from 71.38% and precision to 37.71% from 35.91%. © 2022, Universitas Ahmad Dahlan. All rights reserved.
Program Studi Sarjana Terapan Teknik Elektronika, Universitas Negeri Yogyakarta, Indonesia; Program Studi Informatika, Universitas Ahmad Dahlan, Indonesia
