This paper presents a unified framework for addressing the stability analysis of the hovering condition for a multirotor vehicle. By linearization about a trim condition, a decoupled model made of four dynamic modes is derived. A set of stability derivatives is obtained and the effect on natural dynamic stability of design parameters such as arm dihedral and rotor tilt angles is analyzed. A numerical test case is finally discussed in support of the proposed approach.

de Angelis, E.L. (2018). Stability analysis of a multirotor vehicle hovering condition. AEROSPACE SCIENCE AND TECHNOLOGY, 72, 248-255 [10.1016/j.ast.2017.11.017].

Stability analysis of a multirotor vehicle hovering condition

de Angelis, Emanuele L.
2018

Abstract

This paper presents a unified framework for addressing the stability analysis of the hovering condition for a multirotor vehicle. By linearization about a trim condition, a decoupled model made of four dynamic modes is derived. A set of stability derivatives is obtained and the effect on natural dynamic stability of design parameters such as arm dihedral and rotor tilt angles is analyzed. A numerical test case is finally discussed in support of the proposed approach.
2018
de Angelis, E.L. (2018). Stability analysis of a multirotor vehicle hovering condition. AEROSPACE SCIENCE AND TECHNOLOGY, 72, 248-255 [10.1016/j.ast.2017.11.017].
de Angelis, Emanuele L.
File in questo prodotto:
Eventuali allegati, non sono esposti

I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.

Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11585/619124
 Attenzione

Attenzione! I dati visualizzati non sono stati sottoposti a validazione da parte dell'ateneo

Citazioni
  • ???jsp.display-item.citation.pmc??? ND
  • Scopus 22
  • ???jsp.display-item.citation.isi??? 15
social impact