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• W2734611617 abstract "To solve the flight control problem for a novel x-quadrotors, a dynamic model was developed and analyzed in this paper. A PID-PD controller was designed based on the model to control the x-quadrotors. The PID controller is used in the position loop while the PD controller is used in the attitude loop in dynamic model. Single-loop PID controller is very easy to produce vibration in the flight process. After filtering the pose angles obtained from sensors can reach quite high accuracy, but they still cannot replace the real angles. Therefore, they cannot simply follow the post-filtering pose angles for PID control. In the double-loop PID-PD control, the angles are controlled by the inner loop, and function of the outer loop is to provide the desired angles of the inner loop. The loop feedback of the inner loop guarantees the smoothness of the flight of the x-quadrotor and it will not cause frequent oscillations. The effectiveness of the PID-PD controller was tested with Matlab/Simulink simulation. By comparing the output position data of the three axes and the expectation of them, we found that the output and the expectation are identical. And the simulation results also show that the PID-PD controller is able to stabilize the x-quadrotor robustly with the given parameters." @default.
• W2734611617 created "2017-07-21" @default.
• W2734611617 creator A5014839652 @default.
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• W2734611617 date "2017-02-01" @default.
• W2734611617 modified "2023-09-22" @default.
• W2734611617 title "Dynamic modeling and analyzing for a novel X-quadrotor" @default.
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• W2734611617 doi "https://doi.org/10.1109/ciact.2017.7977292" @default.
• W2734611617 hasPublicationYear "2017" @default.
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