Fault diagnosis and fault-tolerant control and guidance for aerospace vehicles : from theory to application
著者
書誌事項
Fault diagnosis and fault-tolerant control and guidance for aerospace vehicles : from theory to application
（Advances in industrial control）
Springer, c2014
- hardback
大学図書館所蔵 件 / 全1件
-
該当する所蔵館はありません
- すべての絞り込み条件を解除する
注記
Includes bibliographical references and index
内容説明・目次
内容説明
Fault Diagnosis and Fault-Tolerant Control and Guidance for Aerospace demonstrates the attractive potential of recent developments in control for resolving such issues as flight performance, self protection and extended-life structures. Importantly, the text deals with a number of practically significant considerations: tuning, complexity of design, real-time capability, evaluation of worst-case performance, robustness in harsh environments, and extensibility when development or adaptation is required. Coverage of such issues helps to draw the advanced concepts arising from academic research back towards the technological concerns of industry.
Initial coverage of basic definitions and ideas and a literature review gives way to a treatment of electrical flight control system failures: oscillatory failure, runaway, and jamming. Advanced fault detection and diagnosis for linear and linear-parameter-varying systems are described. Lastly recovery strategies appropriate to remaining actuator/sensor/communications resources are developed.
The authors exploit experience gained in research collaboration with academic and major industrial partners to validate advanced fault diagnosis and fault-tolerant control techniques with realistic benchmarks or real-world aeronautical and space systems. Consequently, the results presented in Fault Diagnosis and Fault-Tolerant Control and Guidance for Aerospace, will be of interest in both academic and aerospatial-industrial milieux.
目次
Basic Concepts: Academic State of the Art and Industrial State of Practice.- Robust Fault Detection in Aircraft Control Surface Servo-Loop: Oscillatory Failure Case.- Robust Fault Detection in Aircraft Control Surface Servo-Loop: Runaway and Jamming.- Non-conservative H-infinity/H2 FDD Design: LTI Case.- H-infinity/H2 FDD Design for LPV Case.- An Active Fault-tolerant Flight Control Strategy.- Final Remarks.
「Nielsen BookData」 より