Robust Attitude Control System Design for a Distributed Propulsion Tilt-Wing UAV in Flight State Transition

Siqi Wang, Bifeng Song, Lei He

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

4 Scopus citations

Fingerprint

Dive into the research topics of 'Robust Attitude Control System Design for a Distributed Propulsion Tilt-Wing UAV in Flight State Transition'. Together they form a unique fingerprint.

Engineering

Physics