碩士 / 國立中央大學 / 光機電工程研究所 / 101 / This paper is aiming at a main control system to complete Sound Rocket Ver. 8 re-entry capsule mission. To verify the function, process kinds of environment and function test.
The main control system governs a power management module, a pyrotechnic module, and the following subsystems: Magnetic field sensor subsystem, Gravity and Gyro sensor subsystem, Radio subsystem, Cold Gas Propulsion Control subsystem, and GPS subsystem. With the proper working of the above systems, it is excepted to complete the recovery capsule mission and cold gas de-spin experiment.
To make sure the data correctness and stability of payload, build a system function verification procedure was built, and to verify and validate the data.
| Identifer | oai:union.ndltd.org:TW/101NCU05651009 |
| Date | January 2013 |
| Creators | Yen-ting Chen, 陳彥廷 |
| Contributors | 江士標 |
| Source Sets | National Digital Library of Theses and Dissertations in Taiwan |
| Language | zh-TW |
| Detected Language | English |
| Type | 學位論文 ; thesis |
| Format | 73 |
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