首页> 外文会议>AIAA modeling and simulation technologies conference >Robust Multi-Disciplinary Optimization of Unmanned Entry Capsules
【24h】

Robust Multi-Disciplinary Optimization of Unmanned Entry Capsules

机译:无人入口胶囊的强大多学科优化

获取原文

摘要

Uncertainties in design variables and environmental factors are common in many engineering problems, and they must be taken into account when searching for robust optimal solutions. In robust multi-objective optimization it is common practice to optimize the average performance instead of the nominal objective functions. To compute average performance, and to determine the compliance of the solutions to the constraints, sampling is needed in a neighborhood of each individual and the performance of each sample point must be evaluated. This drives the computational cost of robust optimization up. In this paper we present a repository-based approach that reduces the number of evaluations needed during robust optimization. Unlike most of the approaches available to date, we introduce methods to keep the joint probability density function of the input variables intact when pre-existing points from the repository shall be used. This allows for cheap robust-optimization also in the presence of non-uniform uncertain-variable distributions. The robust optimization of unmanned entry capsules, considering continuous shape-variation models, aerothermodynamics, flight mechanics, and thermal protection system models at the same time is a valuable test-bed for the method presented here. In this paper we discuss the results of minimizing the mass of the capsules while maximizing the internal volume and the re-usability. We demonstrate that using a double-repository archive maintenance scheme it is possible to obtain accurate results and a reduction of the computational cost that is close to 70%, if compared to classical sampling-based methods for robust optimization. The analysis of robust-optimal entry capsules demonstrates that there are design conditions for which small and fully reusable capsules for unmanned entry from low Earth orbits perform as well as capsules with ablative materials, also under uncertainties.
机译:在许多工程问题中,设计变量和环境因素的不确定性是常见的,并且在寻找强大的最佳解决方案时必须考虑它们。在强大的多目标优化中,常常做法是优化平均性能而不是标称目标函数。为了计算平均性能,并确定解决方案对约束的遵守情况,每个单独的邻域都需要采样,并且必须评估每个采样点的性能。这驱动了鲁棒优化的计算成本。在本文中,我们介绍了一种基于存储库的方法,可以减少强大优化期间所需的评估数量。与迄今为止可用的大多数方法不同,我们介绍当使用从存储库的预先存在点时保持输入变量的联合概率密度函数的方法。这允许在存在非均匀不确定可变分布的情况下允许廉价的鲁棒优化。同时考虑连续形状变化模型,空气流动性,飞行机械和热保护系统模型的无人入口胶囊的鲁棒优化是一个有价值的测试床,用于此处的方法。在本文中,我们讨论了最小化胶囊质量的结果,同时最大化内部体积和可重新使用。如果与基于经典采样的鲁棒优化方法相比,我们证明使用双重存储库归档维护方案可以获得准确的结果和降低接近70%的计算成本。鲁棒 - 最佳进入胶囊的分析表明,在低地轨道和低地球轨道上的小型和完全可重复使用的胶囊以及具有烧蚀材料的胶囊,也在不确定度下进行设计条件。

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