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Statistical Risk Estimation for Communication System Design: Development of Optimization Frameworks

机译:通信系统设计的统计风险估算:优化框架的发展

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~1The design of a spacecraft is an evolutionary process that starts from requirements and evolves over time across different design phases. During this process, a lot of changes can happen. They can affect mass and power at component level, at subsystem level, and even at system level. Each spacecraft has to meet overall constraints in terms of mass and power: for this reason, it's important to be sure that the design does not exceed these limitations. Current practice in system modeling deals with this problem by allocating margins on single components and on each of the subsystems. However, a statistical characterization of these fluctuations in mass and power is missing, and the consequence is a design that either is too risky and does not fit the mission constraints, or is too conservative and generates an inefficient utilization of resources. Hence, the objective of this research is to develop a mathematical approach to quantify the likelihood that the design would meet the spacecraft and mission constraints while the design matures. Due to the complexity of the problem and to the different expertise and knowledge required to develop a complete risk model for all the different subsystems, the research is focused on risk estimation for a specific subsystem: communication. Communication constitutes a key design driver in many different spacecraft, and it is also the core in the design of commercial satellite applications. Moreover, the current research aims to be a "proof of concept," which can then be further expanded to the different subsystems, as well as to the whole spacecraft design process. Particularly important in this analysis is the development of optimization frameworks to compare different design architectures, and to select the one that achieves design objectives, like minimal mass and power consumption, while minimizing the risk associated with these same metrics. The article is structured as follows: an overview of the model to perform statistical risk estimation is described, then the mathematical framework for optimization is detailed and applied, and finally results are presented.
机译:〜1宇宙飞船的设计是一种进化过程,从需求开始并随着时间的推移而在不同的设计阶段演变。在此过程中,可能会发生很多变化。它们可以影响组件级别的质量和电力,在子系统级别,甚至在系统级别。每个航天器都必须在质量和权力方面满足整体限制:因此,重要的是要确定设计不超过这些限制。系统建模的当前实践通过分配单个组件和每个子系统的边距来处理此问题。然而,缺失质量和力量的这些波动的统计表征,结果是一种设计,无论是过于危险的,也不适合任务约束,或者过于保守的,并产生资源的低效利用率。因此,这项研究的目的是开发一种数学方法来量化设计在设计成熟时符合航天器和任务约束的可能性。由于问题的复杂性以及为所有不同子系统开发完整的风险模型所需的不同专业知识和知识,该研究专注于特定子系统的风险估计:沟通。通信构成了许多不同的航天器中的关键设计驱动程序,也是商业卫星应用设计中的核心。此外,目前的研究旨在成为“概念证明”,然后可以进一步扩展到不同的子系统,以及整个航天器设计过程。在该分析中特别重要的是开发优化框架,以比较不同的设计架构,并选择实现设计目标,如最小质量和功耗,同时最小化与这些相同度量相关的风险。该物品的结构如下:描述了用于执行统计风险估计的模型的概述,然后详细介绍和应用了优化的数学框架,并且呈现了结果。

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