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Authors
Danesh, Mohammad https://orcid.org/0000-0002-5748-6537
Jalalaei, Amirhossein
Derakhshan, Reza Ebrahimpour
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Article History
Received: 26 July 2022
Revised: 14 December 2022
Accepted: 6 February 2023
First Online: 27 March 2023
Declarations
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: The authors have no competing interests to declare that are relevant to the content of this article.
: The external disturbances considered to evaluate the performance of the quadrotor in tracking the square path are expressed in the following relationships. The simulation results by taking into account the defined disturbances are presented in Figs. , and . As it is clear, the quadrotor will deviate from its initial path over time, and the control algorithms used in the flight control system cannot fully deal with the external disturbances.
