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Case Study Illustrations: a) Spacecraft Structure and Sub-Components b)Spacecraft in Orbit

Case Study Illustrations: a) Spacecraft Structure and Sub-Components b)Spacecraft in Orbit

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... we cap the maximum nodalization of the model with a penalty function, the losses L m and L c force the transfer network to learn to trade-off nodes between faces depending on the incident thermal loads instead of simply predicting a uniform higher or lower nodalization across all faces. Figure 4 shows the structure of the model spacecraft used in this analysis and also illustrates an orbit along which the thermal simulation is conducted. The model spacecraft has two solar arrays and an Earth-pointing protrusion, which along with the optical bench side represents an instrument payload. ...

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