Thrust Pulse Control For UAV Control System Reconfiguration

被引：0

作者：

Zugaj, Marcin ^{[1
]}

Bibik, Przemyslaw ^{[1
]}

Jozefowicz, Karolina ^{[1
]}

机构：

[1] Warsaw Univ Technol, Inst Aeronaut & Appl Mech, Warsaw, Poland

来源：

2016 21ST INTERNATIONAL CONFERENCE ON METHODS AND MODELS IN AUTOMATION AND ROBOTICS (MMAR) | 2016年

关键词：

UAV; recofiguration; control; flight dynamics; AUTOPILOT;

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

A new reconfiguration method using thrust pulse control is proposed in this paper. A reconfigurable closed-loop control system is established for control of a UAV fixed wing aircraft pitch angle via a pulse excitation of thrust in case of elevator failure. The pulse signal parameters are determined by analysis of a nonlinear dynamic model of a UAV aircraft. The model is also used to demonstrate the proposed method. Simulation results show that the aircraft pitch control via thrust pulse excitation can be carried out and satisfactory system performance may be achieved.

引用

页码：708 / 713

页数：6

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