LEADER 01157nam0-2200361---450 001 990008869450403321 005 20190529131448.0 010 $a978-88-8145-122-7 035 $a000886945 035 $aFED01000886945 035 $a(Aleph)000886945FED01 035 $a000886945 100 $a20090625d2008----km-y0itay50------ba 101 0 $aita 102 $aIT 105 $ay-------001yy 200 1 $a<>analisi della redditivitą delle colture agrumicole attraverso l'utilizzo dei dati RICA$fFelicetta Carillo, Paola Doria, Fabio Albino Madau 210 $aRoma$cINEA$d2008 215 $a47 p.$d24 cm 225 1 $a<>quaderni del progetto Piano agrumi$v2 610 0 $aMercati agricoli 610 0 $aAgrumi 676 $a380.141$v20$zita 700 1$aCarillo,$bFelicetta$0432294 701 1$aDoria,$bPaola$0315471 701 1$aAlbino Madau,$bFabio$0432295 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aLG 912 $a990008869450403321 952 $a60 OP. 23/42$b11927$fFAGBC 959 $aFAGBC 996 $aAnalisi della redditivitą delle colture agrumicole attraverso l'utilizzo dei dati RICA$9803546 997 $aUNINA LEADER 03236nam 22006135 450 001 9910739412403321 005 20251113175953.0 010 $a981-16-0439-8 024 7 $a10.1007/978-981-16-0439-3 035 $a(CKB)4100000011797562 035 $a(MiAaPQ)EBC6518443 035 $a(Au-PeEL)EBL6518443 035 $a(OCoLC)1243532696 035 $a(PPN)254726879 035 $a(DE-He213)978-981-16-0439-3 035 $a(EXLCZ)994100000011797562 100 $a20210313d2021 u| 0 101 0 $aeng 135 $aurcnu|||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aControl Allocation for Spacecraft Under Actuator Faults /$fby Qinglei Hu, Bo Li, Bing Xiao, Youmin Zhang 205 $a1st ed. 2021. 210 1$aSingapore :$cSpringer Nature Singapore :$cImprint: Springer,$d2021. 215 $a1 online resource (xviii, 221 pages) 225 1 $aIntelligent Technologies and Robotics Series 311 1 $a981-16-0438-X 327 $aIntroduction -- Spacecraft Model and Control Allocation Formulation -- Null-space based Optimal Control Allocation for Spacecraft Stabilization -- Robust finite-time control allocation under actuator misalignment -- Finite-Time Fault-Tolerant Spacecraft Attitude Control and Control allocation with Torque Saturation -- Fault Tolerant Control Allocation of Spacecraft Using Fault Detection and Diagnosis -- Extended State Observer based Optimal Control Allocation -- Nonlinear Proportional-Derivative Control Incorporating Closed-loop Control Allocation -- Closed-Loop-Based Control Allocation for Spacecraft Attitude Stabilization with Actuator Fault -- Conclusion. 330 $aThis book provides a systematical and comprehensive description of some facets of modeling, designing, analyzing and exploring the control allocation and fault-tolerant control problems for over-actuated spacecraft attitude control system under actuator failures, system uncertainties and disturbances. The book intends to provide a unified platform for understanding and applicability of the fault-tolerant attitude control and control allocation for different purposes in aerospace engineering and some related fields. And it is particularly suited for readers who are interested to learn solutions in spacecraft attitude control system design and related engineering applications. . 410 0$aIntelligent Technologies and Robotics Series 606 $aControl engineering 606 $aRobotics 606 $aAutomation 606 $aAerospace engineering 606 $aAstronautics 606 $aControl, Robotics, Automation 606 $aAerospace Technology and Astronautics 615 0$aControl engineering. 615 0$aRobotics. 615 0$aAutomation. 615 0$aAerospace engineering. 615 0$aAstronautics. 615 14$aControl, Robotics, Automation. 615 24$aAerospace Technology and Astronautics. 676 $a629.4742 700 $aHu$b Qinglei$0852973 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910739412403321 996 $aControl allocation for spacecraft under actuator faults$93552860 997 $aUNINA