Parman, Setyamartana (2009) Finite Element Software Development of a Flexible Satellite Orbiting in Space. In: International Conference on APPLICATIONS AND DESIGN IN MECHANICAL ENGINEERING (ICADME) 2009, 11-13 October 2009, Batu Feringhi, Pulau Pinang.
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Abstract
A computer code to simulate dynamics of flexible satellites orbiting the earth is developed. As the particular model, the satellite consisting of a rigid main body and two symmetrical flexible solar panels is observed. The motion of the solar panels is discretized by using finite element method. For this purpose the solar panels are supposed as a number of rectangular plate elements. The natural frequencies are then studied in order to determine the important modes during its operation.
| Item Type: | Conference or Workshop Item (Paper) |
|---|---|
| Subjects: | T Technology > TL Motor vehicles. Aeronautics. Astronautics |
| Departments / MOR / COE: | Departments > Mechanical Engineering |
| ID Code: | 1089 |
| Deposited By: | Dr Setyamartana Parman |
| Deposited On: | 22 Apr 2010 17:32 |
| Last Modified: | 19 Jan 2017 08:25 |
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