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It is common for Finite Element Model (FEM) validation activities to be carried out in the modal domain; using finite element modal analysis results and modal parameters [...]
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The vibrations that a spacecraft experiences during launch are critical for the safety and integrity of its payload. To simulate the launch, a Coupled Load Analysis (CLA) [...]
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Amongst many sources of microvibration onboard satellites, reaction wheels and momentum wheel assemblies are often considered the most significant. This article presents [...]
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In the recent years, due to the higher-stability requirements imposed by the modern satellites’ payloads, an increasing amount of emphasis is being placed in understand [...]
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Deployable structures are required for many satellite operations, to deploy booms for communications or area deployment for power generation, and many sophisticated mecha [...]
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Reduction of large size Finite Element models is a common technique in dynamic analysis. In particular validation of Finite Element models requires comparison between the [...]
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Highly stable structures that are destined for space use are vulnerable to dimensional stability loss due to random vibration loads experienced during launch and ground t [...]
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Deployable structures are required for many satellite operations, to deploy booms for communications or area deployment for power generation, and many sophisticated mecha [...]
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