03924nam a22005415i 4500001001800000003000900018005001700027007001500044008004100059020003700100024003500137050001300172072001600185072001700201072002300218072001500241072001600256100008400272245012300356250001800479264007200497300006600569336002600635337002600661338003600687347002400723505085600747520109201603650003402695650002502729650002502754650002602779650002702805650005002832650003902882650003602921700008202957700008403039710003403123773002603157776003603183776003603219776003603255856004603291912001403337912001403351999001703365978-981-97-1654-8DE-He21320251030111809.0cr nn 008mamaa240408s2024    si |    s    |||| 0|eng d  a97898197165489978-981-97-1654-87 a10.1007/978-981-97-1654-82doi 4aTL1-4050 7aTRP2bicssc 7aTTDS2bicssc 7aTEC0020002bisacsh 7aTRP2thema 7aTTDS2thema1 aWang, Xingjian.eauthor.4aut4http://id.loc.gov/vocabulary/relators/aut97486810aFault Tolerant Control of Large Civil Aircrafth[electronic resource] /cby Xingjian Wang, Yuwei Zhang, Shaoping Wang.  a1st ed. 2024. 1aSingapore :bSpringer Nature Singapore :bImprint: Springer,c2024.  aVIII, 149 p. 74 illus., 59 illus. in color.bonline resource.  atextbtxt2rdacontent  acomputerbc2rdamedia  aonline resourcebcr2rdacarrier  atext filebPDF2rda0 aChapter 1 Introduction -- Chapter 2 Convex optimization-based fault-tolerant control for dissimilar redundant actuation system of civil aircraft -- Chapter 3 Fault mode probability factor-based fault-tolerant control for dissimilar redundant actuation system -- Chapter 4 Active fault-tolerant control of dissimilar redundant actuation system based on performance degradation reference models -- Chapter 5 Variable-Order Observer-based Fault Tolerant Control for Aircraft with Partial Actuator and Sensor Failures -- Chapter 6 Active Fault-Tolerant Control Strategy of Large Civil Aircraft under Elevator Failures -- Chapter 7 Dynamics and adaptive fault-tolerant flight control under structure damage of horizontal stabilizer -- Chapter 8 Active Fault-Tolerant Control of extreme faults in large aircraft based on propulsion differential -- Appendix.  aThis book provides a comprehensive analysis of fault tolerant control (FTC) for more-electric civil aircraft. FTC is a crucial approach to enhance the reliability and safety of aircraft in the event of actuator, sensor, or structural failures. Engineers and scientists from diverse disciplines, including aeronautics, electrical, mechanical, and control engineering, have been drawn to research on FTC. This book analyzes the impact of faults on performance degradation in dissimilar redundant actuation systems of civil aircraft and presents the FTC methods to ensure reliable actuation and efficient control. Additionally, this book addresses surface damage issues, such as the loss of elevator, horizontal stabilizer, and rudder, by providing representative FTC methods. The book’s major highlight is its comprehensive and systematic approach to FTC design, making it an ideal resource for readers interested in learning about FTC design for civil aircraft. The book benefits researchers, engineers, and graduate students in the fields of FTC, adaptive control, flight control, etc. 0aAerospace engineering.966335 0aAstronautics.966336 0aControl engineering. 0aSystem theory.966519 0aControl theory.96867514aAerospace Technology and Astronautics.96633924aControl and Systems Theory.96586824aSystems Theory, Control.9686761 aZhang, Yuwei.eauthor.4aut4http://id.loc.gov/vocabulary/relators/aut9748691 aWang, Shaoping.eauthor.4aut4http://id.loc.gov/vocabulary/relators/aut9748702 aSpringerLink (Online service)0 tSpringer Nature eBook08iPrinted edition:z978981971653108iPrinted edition:z978981971655508iPrinted edition:z978981971656240uhttps://doi.org/10.1007/978-981-97-1654-8  aZDB-2-ENG  aZDB-2-SXE  c59009d59009