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001435124 001__ 1435124
001435124 003__ OCoLC
001435124 005__ 20230309003837.0
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001435124 007__ cr\cn\nnnunnun
001435124 008__ 210327s2021\\\\si\\\\\\ob\\\\000\0\eng\d
001435124 019__ $$a1242026485$$a1262681149$$a1313550982
001435124 020__ $$a9789811604393$$q(electronic bk.)
001435124 020__ $$a9811604398$$q(electronic bk.)
001435124 020__ $$z9789811604386
001435124 020__ $$z981160438X
001435124 0247_ $$a10.1007/978-981-16-0439-3$$2doi
001435124 035__ $$aSP(OCoLC)1243532696
001435124 040__ $$aEBLCP$$beng$$erda$$epn$$cEBLCP$$dYDX$$dGW5XE$$dOCLCO$$dEBLCP$$dOCLCF$$dUKAHL$$dVLB$$dVT2$$dOCLCQ$$dOCLCO$$dOCLCQ
001435124 049__ $$aISEA
001435124 050_4 $$aTL3260$$b.H8 2021eb
001435124 08204 $$a629.47/42$$223
001435124 1001_ $$aHu, Qinglei,$$eauthor.
001435124 24510 $$aControl allocation for spacecraft under actuator faults /$$cQinglei Hu, Bo Li, Bing Xiao, Youmin Zhang.
001435124 264_1 $$aSingapore :$$bSpringer,$$c[2021]
001435124 264_4 $$c©2021
001435124 300__ $$a1 online resource (xviii, 221 pages)
001435124 336__ $$atext$$btxt$$2rdacontent
001435124 337__ $$acomputer$$bc$$2rdamedia
001435124 338__ $$aonline resource$$bcr$$2rdacarrier
001435124 504__ $$aIncludes bibliographical references.
001435124 50500 $$tIntroduction --$$tMathematical Model of the Attitude Control System --$$tNull-Space Based Optimal Control Allocation for Spacecraft Attitude Stabilization --$$tRobust Finite-Time Control Allocation for Attitude Stabilization Under Actuator Misalignment --$$tFinite-Time Fault-Tolerant Spacecraft Attitude Control with Torque Saturation --$$tExtended State Observer Based Optimal Attitude Robust Control of Spacecraft --$$tSpacecraft Attitude Fault-Tolerant Control Based on Iterative Learning Observer and Control Allocation --$$tNonlinear Proportional-Derivative Control Incorporating Closed-Loop Control Allocation for Spacecraft --$$tClosed-Loop Based Control Allocation for Spacecraft Attitude Stabilization with Actuator Faults --$$tConclusions.
001435124 506__ $$aAccess limited to authorized users.
001435124 520__ $$aThis book provides a systematical and comprehensive description of some facets of modeling, designing, analyzing and exploring the control allocation and fault-tolerant control problems for over-actuated spacecraft attitude control system under actuator failures, system uncertainties and disturbances. The book intends to provide a unified platform for understanding and applicability of the fault-tolerant attitude control and control allocation for different purposes in aerospace engineering and some related fields. And it is particularly suited for readers who are interested to learn solutions in spacecraft attitude control system design and related engineering applications.
001435124 588__ $$aDescription based on print version record.
001435124 650_0 $$aSpace vehicles$$xAttitude control systems.
001435124 650_0 $$aActuators.
001435124 650_6 $$aVéhicules spatiaux$$xSystèmes de commande d'orientation.
001435124 650_6 $$aActionneurs.
001435124 655_0 $$aElectronic books.
001435124 7001_ $$aLi, Bo,$$eeditor.
001435124 7001_ $$aXiao, Bing,$$eeditor.
001435124 7001_ $$aZhang, Youmin,$$d1965-$$eeditor.
001435124 77608 $$iPrint version:$$aHu, Qinglei.$$tControl Allocation for Spacecraft under Actuator Faults.$$dSingapore : Springer Singapore Pte. Limited, ©2021$$z9789811604386
001435124 852__ $$bebk
001435124 85640 $$3Springer Nature$$uhttps://univsouthin.idm.oclc.org/login?url=https://link.springer.com/10.1007/978-981-16-0439-3$$zOnline Access$$91397441.1
001435124 909CO $$ooai:library.usi.edu:1435124$$pGLOBAL_SET
001435124 980__ $$aBIB
001435124 980__ $$aEBOOK
001435124 982__ $$aEbook
001435124 983__ $$aOnline
001435124 994__ $$a92$$bISE