OpenAlex | Optimal control of satellite attitude and its stability based on quaternion parameters

Optimal control of satellite attitude and its stability based on quaternion parameters

Work

Year: 2021

Type: article

Source: Computational methods for differential equations

Authors Mohammad Reza Niknam, Hossein Kheiri, Nadereh Abdi Sobouhi

Institutions Islamic Azad University, Tehran, University of Tabriz, Farhangian University

Cites:

Cited by: 1

Related to: 20

FWCI: 0.121

Citation percentile (by year/subfield): 35.11

Topic: Control and Dynamics of Mobile Robots

Subfield: Control and Systems Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed