Abstract
The aim of this study is to assist the debugging of servo motion control system and the designing of product structure while develo** electric-optic turret of the current UAV’s mission payload. We researched on the electromechanical co-simulation technology for the electric-optic turret stabilized platform by constructing a multi-body dynamic model for the structure, Considering the disturbance of UAV, and designing an inertial servo control system using the speed-loop control to achieve inertial stability. The study implemented the electromechanical co-simulation analysis of the integration of mechanism and the servo control system.
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Zhao, ZY., Liu, A. (2024). Electromechanical Co-simulation for UAV’s Mission Payload. In: Li, S. (eds) Computational and Experimental Simulations in Engineering. ICCES 2023. Mechanisms and Machine Science, vol 146. Springer, Cham. https://doi.org/10.1007/978-3-031-44947-5_75
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DOI: https://doi.org/10.1007/978-3-031-44947-5_75
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