Work

Controllability of spacecraft using only magnetic torques

Year: 2016

Type: article

Abstract: Spacecraft attitude control using only magnetic torques is a time-varying system. Many designs have been proposed using linear quadratic regulator (LQR) and H∞ formulations. The existence of the solutions depends on the controllability of the linear time-varying systems, which has not been established. In this paper, the conditions of controllability for this linear time-varying system is derived.

Source: IEEE Transactions on Aerospace and Electronic Systems

DOI: 10.1109/taes.2015.150520

Author: Yaguang Yang

Institution: United States Nuclear Regulatory Commission

Language: English

Topic: Spacecraft Dynamics and Control

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: green

OpenAlex ID: W2246559928

FWCI: 7.682

Cites: 20

Cited by: 45

Related to: 10