A coordinated turn controller for a fixed-wing aircraft

被引：2

作者：

Corona-Sanchez, Jose J. ^{[1
]}

Guzman Caso, Oscar Roberto ^{[2
]}

Rodriguez-Cortes, H. ^{[1
]}

机构：

[1] Inst Politecn Nacl, Ctr Invest & Estudios Avanzados, Dept Elect Engn, Mexico City, DF, Mexico

[2] Inst Politecn Nacl, ESIME Unidad Ticoman, Mexico City, DF, Mexico

来源：

PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING | 2019年 / 233卷 / 05期

关键词：

Fixed-wing aircraft; lateral-directional dynamics; coordinated turn; control design; flight simulator;

D O I：

10.1177/0954410018761967

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper describes the design of a controller for a fixed-wing aircraft to make it perform coordinated turns. First, a state feedback partial linearization controller drives the airplane to carry out an ideal coordinated turn. A second control loop, inspired by the total heading control system technique, mixes the ailerons and rudder inputs to perform a coordinated turn considering the sideslip dynamics. The control design development gives new insights to establish the fundamental basis for the total heading control system. Simulations in an advanced flight simulator (X-Plane 10) are presented to show the closed-loop system behavior.

引用

页码：1728 / 1740

页数：13

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