.png){kind=icon}
.png){kind=icon}
Return
Bandwidth-constrained disturbance observer design for position control of flapping-wing MAVs with non-minimum-phase dynamics
.png){kind=icon}
OA
AI
A
S
DOI：10.1016/j.conengprac.2026.107099.png)
.png){kind=icon}
.png){kind=icon}
Share.png){kind=icon}
Save
Abstract
En 中文
• System identification reveals non-minimum-phase horizontal dynamics in a hover-capable flapping-wing MAV. • Identified non-minimum phase zero imposes a structural limitation on disturbance observer bandwidth. • Frequency-domain analysis explains waterbed amplification due to NMP-induced phase accumulation. • Experiments demonstrate a bounded feasible cutoff-frequency region. • An intermediate observer bandwidth yields optimal disturbance-stability trade-off.
Keywords:
Flapping-wing UAV
Nonminimum-phase systems
Disturbance observer
Bandwidth limitation
Frequency-domain design
System identification
Robust position control
AI Summary
Key information extracted from the uploaded paper, including a brief overview, abstract, background, key highlights, visual analysis, and future outlook.
Journal
IF:
4.6
Papers:
5.6K
Citations:
1.1W
Organization
No organization information available
Cited Papers