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Design, Specification, and Synthesis...
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Xu, Huan.
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Design, Specification, and Synthesis of Aircraft Electric Power Systems Control Logic.
紀錄類型:
書目-語言資料,印刷品 : Monograph/item
正題名/作者:
Design, Specification, and Synthesis of Aircraft Electric Power Systems Control Logic./
作者:
Xu, Huan.
面頁冊數:
140 p.
附註:
Source: Dissertation Abstracts International, Volume: 74-10(E), Section: B.
Contained By:
Dissertation Abstracts International74-10B(E).
標題:
Engineering, Mechanical. -
電子資源:
http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=3564468
ISBN:
9781303133459
Design, Specification, and Synthesis of Aircraft Electric Power Systems Control Logic.
Xu, Huan.
Design, Specification, and Synthesis of Aircraft Electric Power Systems Control Logic.
- 140 p.
Source: Dissertation Abstracts International, Volume: 74-10(E), Section: B.
Thesis (Ph.D.)--California Institute of Technology, 2013.
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.
ISBN: 9781303133459Subjects--Topical Terms:
783786
Engineering, Mechanical.
Design, Specification, and Synthesis of Aircraft Electric Power Systems Control Logic.
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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.
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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.
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