Decentralized Approaches to Antiwindup Design With Application to Quadrotor Unmanned Aerial Vehicles

被引:31
|
作者
Ofodile, Nkemdilim A. [1 ,2 ]
Turner, Matthew C. [1 ]
机构
[1] Univ Leicester, Dept Engn, Leicester LE1 7RH, Leics, England
[2] Air Force Inst Technol, Kaduna 800001, Nigeria
关键词
Actuator saturation; aerospace applications; antiwindup (AW) compensator design; nonlinear control; quadrotor unmanned air vehicles (UAVs); SYSTEMS; UAV;
D O I
10.1109/TCST.2016.2521799
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 considers the design of structured antiwindup (AW) compensators for open-loop stable plants that themselves have a particular structure: a diagonal dynamic part cascaded with a static invertible part. Two approaches to the design of such compensators are proposed. The first one is a pseudodecentralized AW compensator that is a direct extension of a similar scheme in the literature. The second approach allows the AW compensators to be designed individually for each control channel and, provided that a certain linear program is satisfied, allows the compensators to be implemented in such a way that the nonlinear closed loop is asymptotically stable. The design approaches are applied to a quadrotor UAV, which inspired the work, and results from both simulations and flight tests are reported.
引用
收藏
页码:1980 / 1992
页数:13
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