Robust PID control of quadrotors with power reduction analysis

被引:92
作者
Miranda-Colorado, Roger [1 ]
Aguilar, Luis T. [2 ]
机构
[1] Inst Politecn Nacl, CONACyT, CITEDI, Av Inst Politecn Nacl 1310, Tijuana 22435, Baja California, Mexico
[2] Inst Politecn Nacl, CITEDI, Av Inst Politecn Nacl 1310, Tijuana 22435, Baja California, Mexico
基金
芬兰科学院;
关键词
Robust proportional integral derivative control; Quadrotor unmanned aerial vehicle; Cuckoo search algorithm; Reduction of power consumption; Sliding modes; Quadrotor nonlinear dynamic model; TRAJECTORY TRACKING CONTROL; SLIDING MODE CONTROL; PERFORMANCE; DESIGN; UAV; HELICOPTER; SYSTEMS; FILTER;
D O I
10.1016/j.isatra.2019.08.045
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper presents a novel robust controller applied to a quadrotor vehicle for regulation and trajectory tracking tasks. In the proposed scheme, the quadrotor position is controlled by a proportional integral derivative (PID) controller, while the orientation control is achieved through a model-based controller. The proposed controller is combined with a power reduction methodology, which includes a controller-gains tuning stage using the cuckoo search algorithm, and a minimum jerk trajectory design stage. The performance of the new controller is assessed in a free-disturbance case and under the effect of parametric uncertainty and aero-dynamical disturbances. The new controller is compared against two linear PID controllers and a nonlinear sliding mode-based controller. Numerical simulations demonstrate the superiority of the proposed scheme as well as its robustness against different types of perturbations. Also, it is proven that the power demanded by any controller is reduced when using the power reduction methodology. (C) 2019 ISA. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:47 / 62
页数:16
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