Experimental Validation of an Adaptive Total Energy Control System Strategy for the Longitudinal Dynamics of a Fixed-Wing Aircraft

被引：11

作者：

Brigido-Gonzalez, J. D. ^{[1
]}

Rodriguez-Cortes, H. ^{[2
]}

机构：

[1] Inst Politecn Nacl, Ctr Invest & Estudios Avanzados, Mexico City 07360, DF, Mexico

[2] Inst Politecn Nacl, Ctr Desarrollo Aeroespacial, Mexico City 06010, DF, Mexico

来源：

JOURNAL OF AEROSPACE ENGINEERING | 2016年 / 29卷 / 01期

关键词：

Total energy control system; Fixed-wing aircraft; Adaptive control; FLIGHT CONTROL; DESIGN;

D O I：

10.1061/(ASCE)AS.1943-5525.0000512

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper presents the experimental validation of an adaptive total energy control strategy to regulating the airspeed and the flight path angle of a fixed-wing aircraft. The control strategy is developed from a nonlinear description of the total energy control system approach. An open source computational fluid dynamics software is used to estimate the aerodynamic characteristics of the experimental aircraft. The stability properties are analyzed considering the linearized closed-loop dynamics around an equilibrium point. (C) 2015 American Society of Civil Engineers.

引用

页数：11

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