On the Ability of Sliding Mode and LQR Controllers Optimized with PSO in Attitude Control of a Flexible 4-DOF Satellite with Time-Varying Payload

Publication date: Available online 23 July 2020Source: Advances in Space ResearchAuthor(s): Mahdi Fakoor, Shayesteh Nikpay, Ahmad Kalhor
Source: Advances in Space Research - Category: Science Source Type: research
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