Xi'an Technological University
Subject: Computer Science, Software Engineering
eISSN: 2470-8038
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Keywords : Simulink/Aerosim, dynamic model, flight parameters
Citation Information : International Journal of Advanced Network, Monitoring and Controls. Volume 2, Issue 1, Pages 29-37, DOI: https://doi.org/10.1109/iccnea.2017.17
License : (CC BY-NC-ND 4.0)
Published Online: 07-April-2018
Aiming at the problem of UAV dynamic modeling with high difficulty and poor timeliness, a UAV dynamic model based on Simulink/Aerosim rapid method is established in this paper. Based on the analysis of UAV system internal structure, using Simulink/Aerosim toolbox to build six degrees of freedom dynamic simulation model of unmanned aerial vehicle and the setting of relevant parameters and RTW environment configuration process is analyzed, finally, by analyzing the typical flight parameters of a certain type UAV in ideal environment and wind interference environment, the feasibility and validity of the method is illustrated.
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