Performance analysis of linear periodic systems: application for control of International Space Station

Author

Tchernychev, Andrei ; Alt, Terry ; Harduvel, John

Author_Institution

Boeing Co., Huntington Beach, CA, USA

Volume

4

fYear

1999

fDate

1999

Firstpage

2764

Abstract

We present one approach to conducting a performance analysis of the International Space Station (ISS) being controlled to fly in a specified regime with respect to a solar inertial frame. For the assumed periodic (time-varying) closed-loop system modeling, two stages of the analysis procedure are developed. As the first step, using the so-called Floquet theory, global exponential stability of the closed-loop system is tested. At the next stage, based on the special structures of the closed-loop system and external disturbances, time-domain behavior of the system in the steady state regime is computed without time-domain simulation

Keywords

artificial satellites; asymptotic stability; closed loop systems; control system analysis; linear systems; periodic control; time-varying systems; Floquet theory; International Space Station; external disturbances; global exponential stability; linear periodic systems; performance analysis; periodic time-varying closed-loop system modeling; solar inertial frame; steady state regime; time-domain behavior; Computational modeling; Control systems; International Space Station; Orbits; Performance analysis; Space stations; Stability; Steady-state; Time domain analysis; Time varying systems;

fLanguage

English

Publisher

ieee

Conference_Titel

American Control Conference, 1999. Proceedings of the 1999

Conference_Location

San Diego, CA

ISSN

0743-1619

Print_ISBN

0-7803-4990-3

Type

conf

DOI

10.1109/ACC.1999.786574

Filename

786574