00990cam0-22003611i-450-99000113993040332120130614092301.0000113993FED01000113993(Aleph)000113993FED0100011399320001205d1981----km-y0itay50------baitaIT<<Il >>calcolo sublimestoria dell'analisi matematica da Euler a WeierstrassUmberto BottazziniTorinoBoringhieri1981Lezioni e seminariAnalisi matematicaStoria51520itaBottazzini,Umberto26182ITUNINAREICATUNIMARCBK99000113993040332110-L-721377MA1CPDM-01-001102 CPDMMA102 50 F 53701FINBNMA1FINBN01A0526-0330-03Calcolo sublime344245UNINA01461oam 2200409 450 991071513070332120201229065603.0(CKB)5470000002508709(OCoLC)1139565302(EXLCZ)99547000000250870920200206d1931 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierTests of six symmetrical airfoils in the variable density wind tunnel /by Eastman N. JacobsWashington, [D.C.] :National Advisory Committee for Aeronautics,1931.1 online resource (18 pages, 8 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 385"July, 1931."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 11).AerofoilsWind tunnel testingAerofoils.Wind tunnel testing.Jacobs Eastman N(Eastman Nixon),1902-1987,1387344United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOGPOBOOK9910715130703321Tests of six symmetrical airfoils in the variable density wind tunnel3541400UNINA01104nam 22003973 450 991100845000332120250704110051.097898736678249873667822(CKB)38280616000041(MiAaPQ)EBC32007867(Au-PeEL)EBL32007867(NyNyDIG)DIGEDUNRN0054(OCoLC)1514870245(EXLCZ)993828061600004120250416d2015 uy 0spaur|||||||||||txtrdacontentcrdamediacrrdacarrierAntología de Teatro Rionegrino en la Posdictadura1st ed.Bogota :Universidad Nacional de Río Negro,2015.©2015.1 online resource (296 pages)9789873667060 9873667067 Tossi Mauricio1828226MiAaPQMiAaPQMiAaPQBOOK9911008450003321Antología de Teatro Rionegrino en la Posdictadura4396422UNINA03001nam 22006375 450 991086315320332120251113202605.09783030579579303057957310.1007/978-3-030-57957-9(CKB)4100000011476551(MiAaPQ)EBC6357808(DE-He213)978-3-030-57957-9(PPN)250222043(MiAaPQ)EBC29090494(EXLCZ)99410000001147655120200926d2021 u| 0engurnn|008mamaatxtrdacontentcrdamediacrrdacarrierRobust Discrete-Time Flight Control of UAV with External Disturbances /by Shuyi Shao, Mou Chen, Peng Shi1st ed. 2021.Cham :Springer International Publishing :Imprint: Springer,2021.1 online resource (XVI, 207 p. 97 illus., 62 illus. in color.) Studies in Systems, Decision and Control,2198-4190 ;3179783030579562 3030579565 This book studies selected discrete-time flight control schemes for fixed-wing unmanned aerial vehicle (UAV) systems in the presence of system uncertainties, external disturbances and input saturation. The main contributions of this book for UAV systems are as follows: (i) the proposed integer-order discrete-time control schemes are based on the designed discrete-time disturbance observers (DTDOs) and the neural network (NN); and (ii) the fractional-order discrete-time control schemes are developed by using the fractional-order calculus theory, the NN and the DTDOs. The book offers readers a good understanding of how to establish discrete-time tracking control schemes for fixed-wing UAV systems subject to system uncertainties, external wind disturbances and input saturation. It represents a valuable reference guide for academic research on uncertain UAV systems, and can also support advanced / Ph.D. studies on control theory and engineering. .Studies in Systems, Decision and Control,2198-4190 ;317Computational intelligenceAutomatic controlSystem theoryControl theoryComputational IntelligenceControl and Systems TheorySystems Theory, ControlComputational intelligence.Automatic control.System theory.Control theory.Computational Intelligence.Control and Systems Theory.Systems Theory, Control.629.135Shao Shuyi1230015Chen MouShi Peng1958-MiAaPQMiAaPQMiAaPQBOOK9910863153203321Robust discrete-time flight control of UAV with external disturbances2855189UNINA