Codice QR

The Control Algorithm and Experimentation of Coaxial Rotor Aircraft Trajectory Tracking Based on Backstepping Sliding Mode

In view of the uncertainty of model parameters, the influence of external disturbances and sensor noise on the flight of coaxial rotor aircraft during autonomous flight, a robust backstepping sliding mode control algorithm for the position and attitude feedback control system is studied to solve the...

Descrizione completa

Salvato in:
Dettagli Bibliografici
Autori principali: Jiulong Xu, Yongping Hao, Junjie Wang, Lun Li
Natura: Artigo
Lingua:Inglês
Pubblicazione: MDPI AG 2021-11-01
Serie:Aerospace
Soggetti:
Accesso online:https://www.mdpi.com/2226-4310/8/11/337
Tags: Aggiungi Tag
Nessun Tag, puoi essere il primo ad aggiungerne!!