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Diego Nodar-López

Publications and source records attributed to Diego Nodar-López.

2 recordsLinked to original sources

Integrating Small Satellite Communication in an Autonomous Vehicle Network: A Case for Oceanography

Small satellites and autonomous vehicles have greatly evolved in the last few decades. Hundreds of small satellites have been launched with increasing functionalities, in the last few years. Likewise, numerous autonomous vehicles have been built, with decreasing costs and form-factor payloads. Here we focus on combining these two multifaceted assets in an incremental way, with an ultimate goal of alleviating the logistical expenses in remote oceanographic operations. The first goal is to create a highly reliable and constantly available communication link for a network of autonomous vehicles, taking advantage of the small satellite lower cost, with respect to conventional spacecraft, and its higher flexibility. We have developed a test platform as a proving ground for this network, by integrating a satellite software defined radio on an unmanned air vehicle, creating a system of systems, and several tests have been run successfully, over land. As soon as the satellite is fully operational, we will start to move towards a cooperative network of autonomous vehicles and small satellites, with application in maritime operations, both \textit{in-situ} and remote sensing.

cs.NI↗

Thermal analysis of the electronics of a CubeSat mission

CubeSat satellites are small cube-shaped space platforms that are very popular among academic, research and start-up communities mostly due to their reduced mission costs and short development time. This comes with an easy access to space, which enables high risk missions that would not be feasible otherwise. Thus, most of the subsystems available for these satellites have been adapted to a rather fast development methodology. However, thermal control engineering is still somewhat overlooked due to its complexity and long-term development characteristics. Moreover, since CubeSat projects often rely in commercial off-the-shelf components, it is necessary to understand their necessities in terms of thermal control. The main reason for this is because these components are not originally designed to operate in the space environment, and may degrade faster when operated either under too hot or too cold conditions. In this context, this article presents the results of several thermal analyses and tests conducted over power amplifiers and field-programmable gate array devices, commonly used in CubeSat subsystems and payloads. Passive thermal control methods, mostly based on thermal straps, are explored as potential thermal control solutions due to their low cost and development constraints.

physics.app-ph↗