<abstract xmlns="http://www.w3.org/1999/xhtml">

<p>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.</p>
</abstract>

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.

UAV Dynamic Simulation Model Establishment Method Based on Simulink/Aerosim

International Journal of Advanced Network, Monitoring and Controls

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

{"article-title":"UAV Dynamic Simulation Model Establishment Method Based on Simulink/Aerosim"}

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...

UAV Dynamic Simulation Model Establishment Method Based on Simulink/Aerosim

Publié en ligne: 07 avr. 2018

Pages: 29 - 37

DOI: https://doi.org/10.21307/iccnea.2017.17

Mots clés
Simulink/Aerosim, dynamic model, flight parameters

© 2017 Chen GuoShao et al., published by Sciendo

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

UAV Dynamic Simulation Model Establishment Method Based on Simulink/Aerosim

Publié en ligne: 07 avr. 2018

Pages: 29 - 37

DOI: https://doi.org/10.21307/iccnea.2017.17

Mots clésSimulink/Aerosim, dynamic model, flight parameters

© 2017 Chen GuoShao et al., published by Sciendo

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

Mots clés
Simulink/Aerosim, dynamic model, flight parameters