DocumentCode
1612598
Title
Self-tuning PID control design for quadrotor UAV based on adaptive pole placement control
Author
Jinpeng Yang ; Zhihao Cai ; Qing Lin ; Yingxun Wang
Author_Institution
Nat. Key Lab. of Sci. & Technol. on Aircraft Control, Beihang Univ. Beijing, Beijing, China
fYear
2013
Firstpage
233
Lastpage
237
Abstract
Quadrotor helicopters are an increasingly popular rotorcraft for unmanned aerial vehicle (UAV) platforms. Many groups have worked on quadrotors and realized various controllers and scenarios for it. And PID controller, because of simple structure, good stability and less dependence on the model, plays an important role in quadrotor control. This paper presents an application of Self-tuning PID controller based on adaptive pole placement to a quadrotor. This controller can tune the PID parameters online according to the system change. And the simulation results show that the designed flight controller can achieve accurate control for quadrotor with enough adaptability and robustness.
Keywords
adaptive control; autonomous aerial vehicles; control system synthesis; helicopters; mobile robots; three-term control; UAV platforms; adaptive pole placement control; flight controller design; proportional-integral-derivative control; quadrotor UAV; quadrotor control; quadrotor helicopters; rotorcraft; self-tuning PID control design; Adaptation models; Aerospace control; Equations; Helicopters; Mathematical model; Robustness; Simulation; adaptive control; flight control; quadrotor helicopters; self-tuning PID; simulation verification;
fLanguage
English
Publisher
ieee
Conference_Titel
Chinese Automation Congress (CAC), 2013
Conference_Location
Changsha
Print_ISBN
978-1-4799-0332-0
Type
conf
DOI
10.1109/CAC.2013.6775734
Filename
6775734
Link To Document