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The paper also presents a comparison of various flight control systems and the one, which is designed using H optimization with loop shaping under external wind and aerodynamic disturbances for a six degrees of freedom UAV in which the pitch and angle of attack are controlled by proper canard and el...

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Bibliographic Details
Published inInternational journal of intelligent unmanned systems Vol. 8; no. 3; pp. 141 - 142
Main Authors Rini, Akmeliawati, Kang Taesam, Srigrarom Spot, Budiyono Agus
Format Journal Article
LanguageEnglish
Published Bingley Emerald Group Publishing Limited 01.07.2020
Subjects
Aerodynamics
Algorithms
Altitude
Angle of attack
Datasets
Design
Epigenetics
Flapping
Flight control systems
Navigation systems
Optimization
Pitching moments
Radio signals
Unmanned aerial vehicles
Vehicles
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Summary:The paper also presents a comparison of various flight control systems and the one, which is designed using H optimization with loop shaping under external wind and aerodynamic disturbances for a six degrees of freedom UAV in which the pitch and angle of attack are controlled by proper canard and elevon commands. Besides flight control systems, navigation system is one of very important systems in UAV, especially in the condition whereby GPS systems are unavailable or radio signals are jammed during flights. By incorporating the viscosity effects to the original vortex method, it can eliminate the problem in finding the solution in CFD analysis of unsteady flapping motions for a large number of flapping cycles by controlling the pitching moment amplitude, which grows over time with multiple flapping cycles.
ISSN:2049-6427
2049-6427
DOI:10.1108/IJIUS-07-2020-076