Quadcopter attitude control with vibration reduction by additive-state-decomposition dynamic inversion design with a notch filter
Crossref DOI link: https://doi.org/10.1007/s11071-023-08272-6
Published Online: 2023-02-06
Published Print: 2023-05
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Chen, Lian
Zhang, Jing
Quan, Quan
Text and Data Mining valid from 2023-02-06
Version of Record valid from 2023-02-06
Article History
Received: 22 August 2022
Accepted: 16 January 2023
First Online: 6 February 2023
Declarations
:
: The authors declare that they have no conflict of interest with the present manuscript.