System performance improvement and optimization techniques and their applications in aerospace systems /

Control and Dynamic Systems V54: System Performance Improvement and Optimization Techniques and Their Applications in Aerospace Systems.

Detalles Bibliográficos
Clasificación:Libro Electrónico
Otros Autores: Leondes, Cornelius T.
Formato: Electrónico eBook
Idioma:Inglés
Publicado: San Diego : Academic Press, �1992.
Colección:Control and dynamic systems ; v. 54.
Temas:
Electric power systems > Control.
R�eseaux �electriques (�Energie) > R�egulation.
TECHNOLOGY & ENGINEERING > Automation.
TECHNOLOGY & ENGINEERING > Robotics.
Electric power systems > Control
Acceso en línea:Texto completo

MARC

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245 0 0 |a System performance improvement and optimization techniques and their applications in aerospace systems /  |c edited by C.T. Leondes. 
260 |a San Diego :  |b Academic Press,  |c �1992. 
300 |a 1 online resource (xii, 521 pages) :  |b illustrations 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
338 |a online resource  |b cr  |2 rdacarrier 
490 1 |a Control and dynamic systems ;  |v v. 54 
504 |a Includes bibliographical references and index. 
588 0 |a Print version record. 
505 0 |a Front Cover; System Performance Improvement and Optimization Techniques and Their Applications in Aerospace Systems; Copyright Page; Table of Contents; CONTRIBUTORS; PREFACE; Chapter 1. Techniques for Aircraft Conceptual Design for Mission Performance Comparing Nonlinear Multiobjective Optimization Methods; I. INTRODUCTION; II. GENERAL MULTIOBJECTIVE OPTIMIZATION; III. FORMULATION OF THE MISSION/PERFORMANCE OPTIMIZATION PROBLEM; IV. DESCRIPTION OF THE ANALYSIS SYSTEM FOR MISSION PERFORMANCE; V. DESCRIPTION OF OBJECTIVE FUNCTION FORMULATION METHODS; VI. RESULTS AND DISCUSSION; VII. CONCLUSIONS 
505 8 |a VIII. REFERENCESChapter 2. Optimization of Aerospace Structures using Mathematical Functions for Variable Reduction; I. Introduction; II. Structural Optimization and Variable Reduction; III. Mathematical Functions for Variable Reduction; IV. Optimization of a Wing-Box Structure; V. Further Applications using Mathematical Functions; VI. Recommendations and 'Cook-Book' Methods; VII. Conclusions; VIII. Acknowledgement; IX. References; Chapter 3. Knowledge-Based System Techniques For Pilot Aiding; I. INTRODUCTION; II. BACKGROUND; III. KNOWLEDGE ENGINEERING DESIGN; IV. SYSTEM ARCHITECTURE 
505 8 |a v. KNOWLEDGE CONSTRUCTIONVI. SUMMARY AND CONCLUSIONS; VII. REFERENCES; Chapter 4. Techniques for Optimal Sensor Placement for On- Orbit Modal Identification and Correlation of Large Aerospace System Structures; I. INTRODUCTION; II. TEST-ANALYSIS CORRELATION; III. SENSOR PLACEMENT THEORY; IV. EFFECTS OF SENSOR NOISE1; V� EFFECTS OF ANALYTICAL MODEL ERROR2; VI. CONCLUSION; REFERENCES; Chapter 5. Investigation on the Use of Optimization Techniques for Helicopter Airframe Vibrations Design Studies; I. INTRODUCTION; II. BACKGROUND; III. KEY TASKS IN AIRFRAME OPTIMIZATION 
505 8 |a IV. FORMULATIONS OF THE VIBRATION OPTIMIZATION PROBLEMV. DYNOPT COMPUTER PROGRAM; VI. AIRFRAME DESIGN PROCESS; VII. APPLICATION OF DYNOPT TO A HELICOPTER AIRFRAME; VIII. SUMMARY AND CONCLUDING REMARKS; ACKNOWLEDGEMENT; REFERENCES; APPENDIX; Chapter 6. SIZE-REDUCTION TECHNIQUES FOR THE DETERMINATION OF EFICIENT AEROSERVOELASTIC MODELS; I. INTRODUCTION; II. FREQUENCY-DOMAINEQUATIONS OF MOTION; III. STATE-SPACE EQUATIONS OF MOTION; IV. RATIONAL FUNCTION APPROXIMATIONS; V. APPROXIMATION PROCEDURE; VI. DATA WEIGHTING; VII. RESIDUALIZATION OF STRUCTURAL STATES; VIII. NUMERICAL EXAMPLE 
505 8 |a IX. CONCLUSIONSACKNOWLEDGMENT; REFERENCES; Chapter 7. SENSITIVITY ANALYSIS OF EIGENDATA OF AEROELASTIC SYSTEMS; I. INTRODUCTION; II. TIME-INVARIANT SYSTEMS; III. PERIODIC SYSTEMS; IV� APPLICATIONS; V. SUMMARY; APPENDIX A. EQUATIONS OF MOTION OF HOVERING ROTORS; APPENDIX B. DEFINITION OF MATRICES IN THE EQUATIONS OF MOTION OF THE COUPLED ROTOR-BODY PROBLEM; REFERENCES; Chapter 8. A SIMPLIFIED GENERAL SOLUTION METHODOLOGY FOR TRANSIENT STRUCTURAL DYNAMIC PROBLEMS WITH LOCAL NONLINEARITIES; I. Introduction; II. Modal Transient Solution; III. Simple Structural Deadband 
520 |a Control and Dynamic Systems V54: System Performance Improvement and Optimization Techniques and Their Applications in Aerospace Systems. 
546 |a English. 
650 0 |a Electric power systems  |x Control. 
650 6 |a R�eseaux �electriques (�Energie)  |x R�egulation.  |0 (CaQQLa)201-0079523 
650 7 |a TECHNOLOGY & ENGINEERING  |x Automation.  |2 bisacsh 
650 7 |a TECHNOLOGY & ENGINEERING  |x Robotics.  |2 bisacsh 
650 7 |a Electric power systems  |x Control  |2 fast  |0 (OCoLC)fst00905538 
700 1 |a Leondes, Cornelius T. 
776 0 8 |i Print version:  |t Control and dynamic systems : Volume 54, System performance improvement and optimization techniques and their applications in aerospace systems.  |d San Diego : Academic Press, �1992  |z 0120127547  |w (DLC) 64008027  |w (OCoLC)27694357 
830 0 |a Control and dynamic systems ;  |v v. 54. 
856 4 0 |u https://sciencedirect.uam.elogim.com/science/book/9780120127542  |z Texto completo 

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