It looks like you're offline.
Open Library logo
additional options menu

MARC Record from marc_columbia

Record ID marc_columbia/Columbia-extract-20221130-032.mrc:134234928:6603
Source marc_columbia
Download Link /show-records/marc_columbia/Columbia-extract-20221130-032.mrc:134234928:6603?format=raw

LEADER: 06603cam a22007454a 4500
001 15800573
005 20220507230850.0
006 m o d
007 cr cnu---unuuu
008 060126s2004 flua ob 001 0 eng d
035 $a(OCoLC)ocm63176285
035 $a(NNC)15800573
040 $aN$T$beng$epn$cN$T$dOCLCQ$dYDXCP$dOCLCQ$dVLB$dPUL$dCAI$dDEBBG$dIDEBK$dE7B$dOCLCQ$dHNK$dTXJ$dUV0$dZCU$dUIU$dMYPMP$dEBLCP$dOCLCO$dOCLCQ$dN$T$dOCLCF$dN$T$dOCLCQ$dCRCPR$dOCLCQ$dUIU$dDEBSZ$dOCLCQ$dUAB$dOTZ$dTYFRS$dOCLCQ$dERL$dOCLCQ$dCEF$dUPM$dEZ9$dOCLCQ$dWYU$dS9I$dYDX$dLEAUB$dOCLCQ$dUHL$dOCLCQ$dUKAHL$dOCLCO
019 $a56630360$a171116300$a239617465$a276791588$a506849825$a647586347$a987668095$a991945409$a995025643$a1000437533$a1006796864$a1031050400$a1047531125$a1086878026
020 $a0203180399$q(electronic bk.)
020 $a9780203180396$q(electronic bk.)
020 $a0203298918
020 $a9780203298916
020 $a9780203298916$q(electronic bk.)
020 $a9781134394142
020 $a1134394144
020 $a9781134394098
020 $a1134394098
020 $a9781134394135
020 $a1134394136
020 $z9780415308526
020 $z0415308526$q(cloth)
024 7 $a10.1201/9780203298916$2doi
035 $a(OCoLC)63176285$z(OCoLC)56630360$z(OCoLC)171116300$z(OCoLC)239617465$z(OCoLC)276791588$z(OCoLC)506849825$z(OCoLC)647586347$z(OCoLC)987668095$z(OCoLC)991945409$z(OCoLC)995025643$z(OCoLC)1000437533$z(OCoLC)1006796864$z(OCoLC)1031050400$z(OCoLC)1047531125$z(OCoLC)1086878026
037 $aTF1669$b00004766
050 4 $aTL589.4$b.A33 2004eb
072 7 $aTRA$x002000$2bisacsh
082 04 $a629.135$222
049 $aZCUA
245 00 $aAdvances in dynamics and control /$cedited by S. Sivasundaram.
260 $aBoca Raton, FL :$bChapman & Hall/CRC,$c©2004.
300 $a1 online resource (334 pages) :$billustrations
336 $atext$btxt$2rdacontent
337 $acomputer$bc$2rdamedia
338 $aonline resource$bcr$2rdacarrier
347 $adata file$2rda
490 1 $aNonlinear systems in aviation, aerospace, aeronautics, and astronautics ;$v2
504 $aIncludes bibliographical references and index.
588 0 $aPrint version record.
520 8 $aAnnotation$bPresenting research papers contributed by experts in dynamics and control, Advances in Dynamics and Control examines new ideas, reviews the latest results, and investigates emerging directions in the rapidly-growing field of aviation and aerospace. Exploring a wide range of topics, key areas discussed include: * rotorcraft dynamics * stabilization of unstable aircraft * spacecraft * satellite dynamics and control * missile auto-pilot and guidance design * hybrid systems dynamics and control * structural and acoustic modeling. Impeccably-researched and expertly-written, this text is a valuable reference for graduate students and scientific workers in universities and industry.
505 0 $aFront cover; CONTENTS; CONTRIBUTORS; PREFACE; 1 Global Spacecraft Attitude Control Using Magnetic Actuators; 1 INTRODUCTION; 2 THE MODEL; 3 MAGNETIC FIELD MODEL; 4 STATE FEEDBACK STABILIZATION; 5 STABILIZATION WITHOUT RATE FEEDBACK; 6 SIMULATION RESULTS; 7 CONCLUDING REMARKS; Acknowledgments; REFERENCES; 2 Adaptive Learning Control for Spacecraft Formation Flying; 1 INTRODUCTION; 2 SYSTEM MODEL; 3 PROBLEM FORMULATION; 4 ADAPTIVE LEARNING CONTROLLER; 4.1 Controller Design; 4.2 Stability Analysis; 5 SIMULATION RESULTS; 6 CONCLUSION; Acknowledgments; REFERENCES
505 8 $a3 Spectral Properties of the Generalized Resolvent Operator for an Aircraft Wing Model in Subsonic Airflow1 INTRODUCTION; 2 STATEMENT OF THE PROBLEM; 3 OPERATOR REFORMULATION OF THE PROBLEM; 4 ASYMPTOTIC AND SPECTRAL PROPERTIES OF THE MATRIX DIFFERENTIAL OPERATOR; 5 ASYMPTOTICAL DISTRIBUTION OF AEROELASTIC MODES; 6 STRUCTURE AND PROPERTIES OF MATRIX INTEGRAL OPERATOR; 7 PROPERTIES OF THE ADJOINT OPERATORS AND OPERATOR-VALUED FUNCTIONS; Acknowledgments; REFERENCES; 4 Bifurcation Analysis for the Inertial Coupling Problem of a Reentry Vehicle; 1 INTRODUCTION; 2 EQUATIONS OF MOTION
505 8 $a3 CONTINUATION METHOD4 NUMERICAL RESULTS; 5 RECOVERY FROM A HIGH ROLL-RATE MOTION; 6 CONCLUSION; REFERENCES; 5 Missile Autopilot Design Using Dynamic Fuzzy Gain-Scheduling Technique; 1 INTRODUCTION; 2 AUTOPILOT MODEL AND PERFORMANCE OBJECTIVE; 3 FUZZY DYNAMIC GAIN-SCHEDULED AUTOPILOT; PD Type Controller; 4 RESULTS AND ANALYSIS; 5 CONCLUSIONS; Acknowledgment; REFERENCES; 6 Model Predictive Control of Nonlinear Rotorcraft Dynamics with Application to the XV-15 Tilt Rotor; 1 INTRODUCTION; 2 MODEL PREDICTIVE CONTROL OF NONLINEAR SYSTEMS; 2.1 Control Problem
505 8 $a2.2 Linear Parameter-Varying Approximation2.3 MPC Implementation; 3 APPLICATION TO NONLINEAR VIBRATION CONTROL; 4 APPLICATION TO THE XV-15 TILT ROTOR FLIGHT CONTROL; 4.1 MPC Architectures for FCS; 4.2 Design Procedure; 4.3 Maneuvers for Evaluation; 4.4 Piloted Simulations; 5 CONCLUSIONS; Acknowledgments; REFERENCES; 7 New Development of Vector Lyapunov Functions and Airplane Control Synthesis; 1 INTRODUCTION; 2 VECTOR LYAPUNOV FUNCTION CONCEPT 2.1 Semidefinite and Definite Time-Independent Vector Functions
505 8 $a2.2 Semidefinite and Definite Time-Dependent Vector Functions Definition 3 A vector function v(.) :2.3 Kinds of Vector Lyapunov Functions; 3 SYSTEM DESCRIPTION; 4 CONTROL SYNTHESIS: EXPONENTIAL STABILITY 4.1 Sliding Set; 4.2 Stabilizing Control Problem Statement Problem 8 Synthesize control u(.) so as to ensure that both (i) and (ii) hold for every; 4.3 Stabilizing Control Problem Solution; 5 CONTROL SYNTHESIS: OUTPUT TRACKING AND ASYMPTOTIC STABILITY 5.1 Tracking and Stabilizing Control Problem Statement; 6 CONCLUSION; REFERENCES
650 0 $aFlight control.
650 0 $aAerodynamics.
650 6 $aSystèmes de commande (Vol)
650 6 $aAérodynamique.
650 7 $aaerodynamics.$2aat
650 7 $aTRANSPORTATION$xAviation$xGeneral.$2bisacsh
650 7 $aAerodynamics.$2fast$0(OCoLC)fst00798195
650 7 $aFlight control.$2fast$0(OCoLC)fst00927313
655 0 $aElectronic books.
655 4 $aElectronic books.
700 1 $aSivasundaram, S.
776 08 $iPrint version:$tAdvances in dynamics and control.$dBoca Raton, FL : Chapman & Hall/CRC, ©2004$z0415308526$w(DLC) 2003070019$w(OCoLC)53926750
830 0 $aNonlinear systems in aviation, aerospace, aeronautics, astronautics ;$vv. 2.
856 40 $uhttp://www.columbia.edu/cgi-bin/cul/resolve?clio15800573$zTaylor & Francis eBooks
852 8 $blweb$hEBOOKS