Output Feedback Control for a Quadrotor Aircraft Using an Adaptive High Gain Observer
Crossref DOI link: https://doi.org/10.1007/s12555-019-0944-6
Published Online: 2020-02-04
Published Print: 2020-06
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Flores, Gerardo
González-Huitron, V.
RodrĂguez-Mata, A. E. http://orcid.org/0000-0002-0262-420X
Text and Data Mining valid from 2020-02-04
Version of Record valid from 2020-02-04
Article History
Received: 28 December 2018
Revised: 15 August 2019
Accepted: 21 October 2019
First Online: 4 February 2020