scholarly journals Design and Implementation of UAV’s Flight Control System Test Platform

2019 ◽  
Vol 677 ◽  
pp. 052056
Author(s):  
Yang Liu ◽  
Xuetao Tian
Keyword(s):  
Control System ◽  
Flight Control ◽  
Flight Control System ◽  
Design And Implementation ◽  
Test Platform

scholarly journals Improved Design and Implementation of Automatic Flight Control System (AFCS) for a Fixed Wing Small UAV

2018 ◽  
Vol 27 (3) ◽  
pp. 882-890 ◽  
Author(s):  
A. E. A. Elbanna ◽  
T. H. M. Soliman ◽  
A. N. Ouda ◽  
E. M. Hamed
Keyword(s):  
Control System ◽  
Flight Control ◽  
Flight Control System ◽  
Design And Implementation ◽  
Small Uav ◽  
Improved Design

Design and Implementation of a Dual-Redundant Flight Control System for a Miniature Autonomous Helicopter

2013 ◽  
Vol 278-280 ◽  
pp. 1723-1728
Author(s):  
Qiang Wang ◽  
Bing Zhu ◽  
Peng Liu
Keyword(s):  
Control System ◽  
Flight Control ◽  
Design Procedure ◽  
Control Architecture ◽  
Control Law ◽  
Systematic Design ◽  
Flight Control System ◽  
Flight Tests ◽  
Design And Implementation ◽  
Autonomous Helicopter

This paper present the design and implementation of a dual-redundant flight control system for a miniature autonomous helicopter, named SRD-Heli. The systematic design procedure includes hardware integration, flight control law, exchange scheme, as well as experimental evaluation. A dual-redundant control architecture is adopted to construct the flight control system for the helicopter. The control architecture is composed by (1) an active flight control law designed for the active computer, which works in normal condition, (2) a standby flight control law to effectively control the helicopter by standby computer in fault condition. The result of actual flight tests shows that the flight control system is capable of achieving the desired performance.

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