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

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3 Author(s)
A. Tchernychev ; Boeing Co., Huntington Beach, CA, USA ; T. Alt ; J. Harduvel

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

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American Control Conference, 1999. Proceedings of the 1999  (Volume:4 )

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