Integration of Computer Subsystems and Power Subsystem for Micro-satellite

機構典藏 > College of Engineering > Graduate Institute & Department of Mechanical and Electro-Mechanical Engineering > Journal Article > Item 987654321/100580

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Title:	Integration of Computer Subsystems and Power Subsystem for Micro-satellite
Authors:	Huan-Jung Lin1, Zuu-Chang Hong **,2, Tzung-Hang Lee2, and Yung-Chuang Wen2
Contributors:	機械與機電工程學系暨研究所
Keywords:	微衛星;衛星電腦;電源系統;飛行軟體;Microsatellite;Onboard computer;Power supply unit;Flight software
Date:	2012
Issue Date:	2015-03-06 19:15:52 (UTC+8)
Abstract:	In this paper, the integration among on-board computer-MPC555, power supply unit, and ground station is presented. The design is to execute the mission performance under the satellite orbiting mode, includes supervising and managing satellite operation, handling and archiving information and message, receiving and executing the ground station command and the satellite bursting incident. Where the multi-task and real-time functions of an embedded system are accomplished, then the satellite flight software is established. The flight software includes initialization and autonomous operation of onboard computer which performs several tasks of satellite operation to meet mission requirement. Under operation mode, these tasks are capable of monitoring satellite’s health data, power supply unit , GPS status and handling incident events.
Relation:	Journal of Aeronautics, Astronautics and Aviation, Series B, 44(1), pp.001-008
Appears in Collections:	[Graduate Institute & Department of Mechanical and Electro-Mechanical Engineering] Journal Article

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