Pandit, Jiwan Kumar and Mahapatra, Roy D and Pandiyan, R (2016) Modal Analysis of Power Electronics Module of Spacecraft and its Health Monitoring - An Approach. In: 12th International Conference on Vibration Problems (ICOVP), DEC 14-17, 2015, Guwahati, INDIA, pp. 283-288.
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The spacecraft launch environment is quite harsh which can damage the spacecraft electronics. The high intensity vibrations occurring during this phase are transmitted to the spacecraft structures and its electronic equipment. The high intensity vibrations can be sensed using flexible nano sensors and these inputs could be used by actuators to safeguard the spacecraft electronics. (C) 2016 The Authors. Published by Elsevier Ltd.
|Item Type:||Conference Proceedings|
|Additional Information:||Copy right for this article belongs to the ELSEVIER SCIENCE BV, SARA BURGERHARTSTRAAT 25, PO BOX 211, 1000 AE AMSTERDAM, NETHERLANDS|
|Department/Centre:||Division of Mechanical Sciences > Aerospace Engineering (Formerly, Aeronautical Engineering)|
|Date Deposited:||07 Dec 2016 06:05|
|Last Modified:||07 Dec 2016 06:05|
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