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Advances in aerospace systems dynamics and control systems . Part 2 of 3 /

Control and Dynamic Systems V32: Advances in Aerospace Systems Dynamics and Control Systems Part 2 of 3.

Detalles Bibliográficos
Clasificación:Libro Electrónico
Otros Autores: Leondes, Cornelius T.
Formato: Electrónico eBook
Idioma:Inglés
Publicado: San Diego : Academic Press, 1990.
Colección:Control and dynamic systems ; v. 32.
Temas:
Acceso en línea:Texto completo

MARC

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245 0 0 |a Advances in aerospace systems dynamics and control systems .  |n Part 2 of 3 /  |c edited by C.T. Leondes. 
260 |a San Diego :  |b Academic Press,  |c 1990. 
300 |a 1 online resource (xiii, 280 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 : advances in theory and applications ;  |v v. 32 
504 |a Includes bibliographical references and index. 
588 0 |a Print version record. 
505 0 |a Front Cover; Advances in Aerospace Systems Dynamics and Control Systems, Part 2 of 3; Copyright Page; Table of Contents; CONTRIBUTORS; PREFACE; Chapter 1. Practical Considerations in Optimal and 4-Dimensional Flight Management Computations; I. Flight Management Systems Background; II. A Simulation Study; III. Optimum Cost Index Search; IV. Fine Speed Adjustment; V. Wind Forecast Error Compensation; VI. Conclusions; References; Chapter 2. Optimal Reduced-Order Subspace-Observer Design with a Frequency-Domain Error Bound; I. Introduction; II. Notation and Definitions 
505 8 |a Chapter 4. Parameter Identification in Distributed StructuresI. Introduction; II. Equation of Motion; III. The Differential Eigenvalue Problem; IV. Solution of the Eigenvalue Problem by Approximate Methods; V. Finite Element-Based Parameter Identification; VI. A Perturbation Technique for Parameter Identification; VII. A Rayleigh-Ritz Type Parameter Identification; VIII. Modal Identification of Self-Adjoint Systems; IX. An Inclusion Principle for Parameter Identification; X. Summary; References; Chapter 5. Combined Structural and Control Optimization: A Steepest Descents Approach 
505 8 |a I. IntroductionII. A Specific Combined Structural and Control Optimization Problem; III. The Numerical Algorithm; IV. The 10-Bar Truss; V. Simulation Preliminaries; VI. Simulation Results; VII. Controlled System Response; VIII. Further Optimization Results; IX. Conclusion; References; Chapter 6. An Asymptotic Perturbation Method for Nonlinear Optimal Control Problems; I. Introduction; II. Optimal Control Formulation; III. An Asymptotic Perturbation Method: The Pedestrian Expansion; IV. Solution of the Nonhomogenous Equations; V. Determination of the Initial Costates 
505 8 |a VI. Recursive Solution for the State/Costate TrajectoriesVII. Illustrative Examples; VIII. Conclusions; References; Chapter 7. Reliability Issues in Structural Control; I. Introduction; II. Equations of Motion; III. Robust Control Design; IV. Component Failure Detection; V. Optimal Allocation of Sensors, Actuators, and Their Backups; VI. Future Directions; Appendix.Methods for Extracting Model Coordinates from the System Output; References; Chapter 8. Control Law Synthesis and Stability Robustness Improvement Using Constrained Optimization Techniques; I. Introduction; II. Equations of Motion 
520 |a Control and Dynamic Systems V32: Advances in Aerospace Systems Dynamics and Control Systems Part 2 of 3. 
546 |a English. 
650 0 |a Control theory. 
650 0 |a Aerodynamics. 
650 0 |a System analysis. 
650 0 |a Flight control. 
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650 6 |a Th�eorie de la commande.  |0 (CaQQLa)201-0012168 
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650 7 |a Control theory.  |2 fast  |0 (OCoLC)fst00877085 
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650 7 |a System analysis.  |2 fast  |0 (OCoLC)fst01141385 
700 1 |a Leondes, Cornelius T. 
776 0 8 |i Print version:  |t Advances in aerospace systems dynamics and control systems . Part 2 of 3.  |d San Diego : Academic Press, 1990  |z 0120127326  |w (DLC) 64008027 
830 0 |a Control and dynamic systems ;  |v v. 32. 
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