Robust Guidance Strategy for Target. Circulation by Controlled UAV

被引：24

作者：

Domes Olavo, Jose Lucas ^{[1
]}

Thums, Goncalo Daniel ^{[2
]}

Jesus, Tales Argolo ^{[3
]}

De Araujo Pimenta, Luciano Cunha ^{[4
]}

Borges Torres, Leonardo Antonio ^{[4
]}

Palhares, Reinaldo Martinez ^{[5
]}

机构：

[1] Univ Fed Minas Gerais, Grad Program Elect Engn, Elect Engn, Belo Horizonte, MG, Brazil

[2] Univ Fed Minas Gerais, Grad Program Elect Engn, Belo Horizonte, MG, Brazil

[3] Fed Ctr Technol Educ, Dept Comp, Belo Horizonte, MG, Brazil

[4] Univ Fed Minas Gerais, Dept Elect Engn, Elect Engn, Belo Horizonte, MG, Brazil

[5] Univ Fed Minas Gerais, Dept Elect Engn, Belo Horizonte, MG, Brazil

来源：

IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 2018年 / 54卷 / 03期

关键词：

PATH-FOLLOWING CONTROL; COORDINATED STANDOFF TRACKING; UNMANNED AERIAL VEHICLES; TRAJECTORY TRACKING; ALGORITHMS; NAVIGATION; AIRCRAFT; SYSTEMS; CURVES; WIND;

D O I：

10.1109/TAES.2018.2793058

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

A controlled fixed-wing unmanned aerial vehicle is modeled as a simplified low-dimensional nonlinear dynamical system with additive disturbances. The guidance strategy presented, considering simultaneously inputs and states constraints, is shown to be robust to additive perturbations representing norm-bounded uncertainties associated with modeling errors resulting front the lower order model approximation, together with unknown but limited atmospheric disturbances. Mathematical proofs arc provided ensuring robustness in achieving target circulation with a minimum prescribed accuracy.

引用

页码：1415 / 1431

页数：17

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