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:无人驾驶舱的稳健的多学科优化

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:设计变量和环境因素的不确定性在许多工程问题中都很常见,在寻找可靠的最佳解决方案时必须将它们考虑在内。在鲁棒的多目标优化中,通常的做法是优化平均性能而不是名义目标函数。为了计算平均性能,并确定解决方案是否符合约束条件,需要在每个个体附近进行采样,并且必须评估每个采样点的性能。这将提高鲁棒优化的计算成本。在本文中,我们提出了一种基于存储库的方法,该方法减少了鲁棒优化期间所需的评估次数。与迄今可用的大多数方法不同,我们将介绍一些方法,当应使用存储库中的预先存在的点时,可保持输入变量的联合概率密度函数不变。这也允许在存在非均匀不确定变量分布的情况下进行廉价的鲁棒优化。同时考虑连续形状变化模型,空气动力学,飞行力学和热保护系统模型的无人驾驶舱的鲁棒优化是此处介绍的方法的宝贵试验平台。在本文中,我们讨论了最小化胶囊质量,同时最大化内部容积和可重复使用性的结果。我们证明,与用于稳健性优化的经典基于采样的方法相比,使用双存储库档案维护方案可以获取准确的结果,并减少接近70%的计算成本。鲁棒最佳进入舱的分析表明,在某些设计条件下,小型和完全可重复使用的低空轨道无人驾驶舱以及具有烧蚀性材料的舱也具有不确定性。

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