Enhanced Thermal Control in Space Radiators: An SQP-Based Optimization Approach
Keywords:
Heat dissipation, Optimization, Radiation cooling, Spacecraft thermal con-trol, Successive Quadratic Programming (SQP)Abstract
Under complex environmental conditions, the cooling process will be significantly enhanced if the detector is kept at an optimal level determined by the thermal index of control. The area and configuration of the detector area in the space ultraviolet imager used in conjunction with the methodology utilised to upgrade the cooling effectiveness of the radiation cooler design are further refined by using successive quadratic algorithms that are aimed towards iterative optimisation of parameters associated with the design. The ultraviolet space imager was associated with a physical model and the thermal simulation model: a defined objective function was detector temperature.
DOI: https://doi.org/10.24321/2454.8669.202602
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