Work

Vibration Suppression of a Flexible Appendage and Pitch Angle Fuzzy Regulation of a Spacecraft

Year: 2025

Type: article

Source: SAE International Journal of Aerospace

DOI: 10.4271/01-18-01-0004

Author: Mohamed Bahita

Institution: University of Constantine 3

Language: English

Topic: Spacecraft Dynamics and Control

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W4407166342

FWCI:

Cites: 24

Cited by:

Related to: 10