Design methods, devices, and computer programs for aerospace optical payloads

Abstract

This disclosure relates to the field of aerospace technology, and more specifically, to a design method, apparatus, and computer program product for aerospace optical payloads. The design method for aerospace optical payloads includes: determining the emphasis dimensions of the optical payload to be designed based on received mission requirements, and determining optical weights, mechanical weights, and thermal control weights based on the emphasis dimensions; determining a performance optimization objective function based on the optical weights, mechanical weights, and thermal control weights, as well as optical, mechanical, and thermal control indicators; performing simulation design of the optical payload based on a simulation model and the mission requirements, and optimizing the simulation design at least based on the performance optimization objective function.

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