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Design, Specification, and Synthesis of Aircraft Electric Power Systems Control Logic.

机译:飞机电力系统控制逻辑的设计,规范和综合。

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摘要

Cyber-physical systems integrate computation, networking, and physical processes. Substantial research challenges exist in the design and verification of such large-scale, distributed sensing, actuation, and control systems. Rapidly improving technology and recent advances in control theory, networked systems, and computer science give us the opportunity to drastically improve our approach to integrated flow of information and cooperative behavior. Current systems rely on text-based specifications and manual design. Using new technology advances, we can create easier, more efficient, and cheaper ways of developing these control systems.;This thesis will focus on design considerations for system topologies, ways to formally and automatically specify requirements, and methods to synthesize reactive control protocols, all within the context of an aircraft electric power system as a representative application area. This thesis consists of three complementary parts: synthesis, specification, and design. The first section focuses on the synthesis of central and distributed reactive controllers for an aircraft elec- tric power system. This approach incorporates methodologies from computer science and control. The resulting controllers are correct by construction with respect to system requirements, which are formulated using the specification language of linear temporal logic (LTL). The second section addresses how to formally specify requirements and introduces a domain-specific language for electric power systems. A software tool automatically converts high-level requirements into LTL and synthesizes a controller.;The final sections focus on design space exploration. A design methodology is proposed that uses mixed-integer linear programming to obtain candidate topologies, which are then used to synthesize controllers. The discrete-time control logic is then verified in real-time by two methods: hardware and simulation. Finally, the problem of partial observability and dynamic state estimation is explored. Given a set placement of sensors on an electric power system, measurements from these sensors can be used in conjunction with control logic to infer the state of the system.
机译:网络物理系统集成了计算,网络和物理过程。在设计和验证此类大规模,分布式传感,致动和控制系统方面,存在重大研究挑战。快速改进的技术以及控制理论,网络系统和计算机科学的最新进展为我们提供了极大地改进我们集成信息流和协作行为方法的机会。当前的系统依赖于基于文本的规范和手动设计。利用新技术的进步,我们可以创建更轻松,更高效,更便宜的控制系统开发方法。本文将重点研究系统拓扑的设计注意事项,正式和自动指定要求的方法以及无功控制协议的综合方法,所有这些都以飞机电力系统为代表的应用领域。本文由三个互补部分组成:综合,规范和设计。第一部分着重于飞机电力系统的中央和分布式无功控制器的综合。这种方法结合了计算机科学和控制学的方法论。由此产生的控制器在结构上相对于系统要求是正确的,系统要求是使用线性时间逻辑(LTL)的规范语言制定的。第二部分介绍如何正式规定要求,并介绍电力系统的特定领域语言。软件工具会自动将高级需求转换为LTL并合成控制器。最后几节着重于设计空间探索。提出了一种设计方法,该方法使用混合整数线性规划来获取候选拓扑,然后将其用于合成控制器。然后,通过两种方法实时验证离散时间控制逻辑:硬件和仿真。最后,探讨了局部可观性和动态状态估计的问题。给定传感器在电力系统上的放置位置,可以将这些传感器的测量值与控制逻辑结合使用以推断系统状态。

著录项

  • 作者

    Xu, Huan.;

  • 作者单位

    California Institute of Technology.;

  • 授予单位 California Institute of Technology.;
  • 学科 Engineering Aerospace.;Engineering System Science.;Computer Science.;Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 2013
  • 页码 140 p.
  • 总页数 140
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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