Gust Load Alleviation Control Strategies for Large Civil Aircraft through Wing Camber Technology

Gust Load Alleviation Control Strategies for Large Civil Aircraft through Wing Camber Technology

This paper introduces three new gust load alleviation control strategies, which are based on variable camber technology, to achieve the design requirements for the safety, economy, and comfort of modern civil aircraft. These strategies involve adjusting the inner and outer flap differential of wings...

Full description

Bibliographic Details
Main Authors: Shanshan Zhang, Yueheng Qiu, Junshuai Sun, Ban Wang, Zhenghong Gao
Format: Article
Language:English
Published: MDPI AG 2024-06-01
Series:Actuators
Subjects:
gust load alleviation control
wing camber
civil aircraft
stepped cruise flight
logic design
Online Access:https://www.mdpi.com/2076-0825/13/6/229

Internet

https://www.mdpi.com/2076-0825/13/6/229

Similar Items