Performance of LIPS III Attitude Control System

The LIPS III satellite is a spin stabilized sun tracking space platform who's primary mission is to test new space power sources. The attitude control system has two modes of operation, hydrazine gas jet for large attitude errors and an electromagnetic torque rod for nominal operations. The control law will be discussed and examples of inflight data will be given.

Authors

Robert L. Burdett (ORCID: https://orcid.org/0000-0003-2484-3646)
R.W. Conway

Institutions

United States Naval Research Laboratory (US)
Honeywell (United States) (US)

Publication Details

Journal: Digital Commons - USU (Utah State University)
Published: 2025-09-10
DOI: https://doi.org/10.26077/bme6-ht12
Primary Topic: Inertial Sensor and Navigation
Type: article

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article

Performance of LIPS III Attitude Control System

Robert L. Burdett, R.W. Conway

Sep 10, 2025

1 links

Digital Commons - USU (Utah State University)

Inertial Sensor and Navigation

article

Performance of LIPS III Attitude Control System

Robert L. Burdett, R.W. Conway

September 10, 2025article en

Abstract

Digital Commons - USU (Utah State University)

United States Naval Research Laboratory (US), Honeywell (United States) (US)

Inertial Sensor and Navigation

DOI Open Access PDF OpenAlex

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Performance of LIPS III Attitude Control System — Robert L. Burdett, R.W. Conway · Digital Commons - USU (Utah State University) (2025) | TGRS Research Map | TGRS