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Design procedure of chattering attenuation sliding mode attitude control of a satellite system (2014)
Conference Proceeding
Nemati, H., & Hokamoto, S. (2014). Design procedure of chattering attenuation sliding mode attitude control of a satellite system

This study presents a design procedure for a new robust nonlinear control algorithm based on the theory of the terminal sliding mode (TSM) to control the attitude of a satellite system. Since the traditional TSM controllers include a discontinuous fu... Read More about Design procedure of chattering attenuation sliding mode attitude control of a satellite system.

New Continuous Sliding Mode Design for Spacecraft Attitude Control (2014)
Presentation / Conference
Nemati, H., Oishi, M., Kobayashi, N., Nakata, R., & Hokamoto, S. (2014, July). New Continuous Sliding Mode Design for Spacecraft Attitude Control. Paper presented at 24th Workshop on JAXA Astrodynamics and Flight Mechanics 2014, Sagamihara, Kanagawa, Japan

New Chattering Attenuation Sliding Mode Control of a Flexible Spacecraft (2014)
Journal Article
Nemati, H., & Hokamoto, S. (2014). New Chattering Attenuation Sliding Mode Control of a Flexible Spacecraft. Transactions of the Japan Society for Aeronautical and Space Sciences, 12(ists29), Pd_71-Pd_77. https://doi.org/10.2322/tastj.12.pd_71

An improved sliding mode control (SMC) strategy for the attitude control problem of a nonlinear spacecraft with an elastic appendage is investigated. Since conventional sliding mode controllers include a discontinuous function, a significant problem... Read More about New Chattering Attenuation Sliding Mode Control of a Flexible Spacecraft.