首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering >Conceptual interplanetary space mission design using multi-objective evolutionary optimization and design grammars
【24h】

Conceptual interplanetary space mission design using multi-objective evolutionary optimization and design grammars

机译:使用多目标进化优化和设计语法的概念性行星际太空任务设计

获取原文
获取原文并翻译 | 示例
       

摘要

Conceptual design optimization (CDO) is a technique proposed for the structured evaluation of different design concepts. Design grammars provide a flexible modular modelling architecture. The model is generated by a compiler based on predefined components and rules. The rules describe the composition of the model; thus, different models can be optimized by the CDO in one run. This allows considering a mission design including the mission analysis and the system design. The combination of a CDO approach with a model based on design grammars is shown for the concept study of a near-Earth asteroid mission. The mission objective is to investigate two asteroids of different kinds. The CDO reveals that a mission concept using two identical spacecrafts flying to one target each is better than a mission concept with one spacecraft flying to two asteroids consecutively.
机译:概念设计优化(CDO)是一种用于对不同设计概念进行结构化评估的技术。设计语法提供了灵活的模块化建模架构。该模型由编译器基于预定义的组件和规则生成。规则描述了模型的组成;因此,CDO可以一次运行优化不同的模型。这允许考虑任务设计,包括任务分析和系统设计。 CDO方法与基于设计语法的模型相结合,用于近地小行星任务的概念研究。任务目标是研究两种不同类型的小行星。 CDO揭示了使用两个相同的航天器分别飞行到一个目标的任务概念要好于一个连续飞行到两个小行星的航天器的任务概念。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号