Payload Swing Attenuation of a Fully-Actuated Hexacopter via Extended High Gain Observer Based Adaptive Sliding Control - CNRS - Centre national de la recherche scientifique Access content directly
Conference Papers Year :
Not file

Dates and versions

hal-03561696 , version 1 (08-02-2022)

Identifiers

Cite

Jorge Arizaga, Herman Castaneda, Pedro Castillo Garcia. Payload Swing Attenuation of a Fully-Actuated Hexacopter via Extended High Gain Observer Based Adaptive Sliding Control. International Conference on Unmanned Aircraft Systems (ICUAS 2021), Jun 2021, Athens, Greece. pp.901-908, ⟨10.1109/ICUAS51884.2021.9476819⟩. ⟨hal-03561696⟩
16 View
0 Download

Altmetric

Share

Gmail Facebook Twitter LinkedIn More