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Advances in aerospace systems dynamics and control systems. advances in theory and applications / Part 3 of 3 :
Control and Dynamic Systems V33: Advances in Aerospace Systems Dynamics and Control Systems Part 3 of 3.
| Clasificación: | Libro Electrónico |
|---|---|
| Otros Autores: | |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
San Diego :
Academic Press,
�1990.
|
| Colección: | Control and dynamic systems ;
v. 33. |
| 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 3 of 3 : |b advances in theory and applications / |c edited by C.T. Leondes. |
| 246 | 3 | |a Advances in aerospace systems dynamics and control systems, Part 3. | |
| 260 | |a San Diego : |b Academic Press, |c �1990. | ||
| 300 | |a 1 online resource (xiv, 305 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. 33 | |
| 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 3 of 3; Copyright Page; Table of Contents; CONTRIBUTORS; PREFACE; Chapter 1. Sensor Failure Detection for Jet Engines; I. Introduction; II. Analytical Redundancy Technology Base; III. Analytical Redundancy Technology Development; IV. Analytical Redundancy Technology Assessment; V. Concluding Remarks; References; Chapter 2. Human Response Models for Interpretive Tasks; I. Introduction; II. Teleoperator Response Modeling; III. Pliancy of the Decision Directed Model; IV. Operator Response Characteristics. | |
| 505 | 8 | |a v. ConclusionsReferences; Chapter 3. Decoupled Flight Control via a Model-Following Technique Using the Euler Operator; I. Introduction; II. Discrete-Time Models and Their Properties; III. Model-Following Controller Design; IV. Model-Following Control Using Plant Output; V. Decoupled Control Configured Vehicle Flight Control; VI. Conclusions; Appendix. FORTRAN Subroutines; References; Chapter 4. Advances in Digital Signal Processing; I. Introduction; II. Multirate Digital Filter Specifications; III. Criteria for Design of Multirate Filters; IV. Multirate Filter Design. | |
| 505 | 8 | |a v. Statement of the ProblemVI. Solution by the Method of Lagrange Multipliers; VII. Maximally Flat Multirate Finite Impulse Response Digital Filters; VIII. Bandpass Finite Impulse Response Digital Filters; IX. Passband Fine Tuning; X. Filter Design Algorithm; XI. Design Examples; XII. Summary; Appendix. Derivation of Equation (54); References; Chapter 5. Methodology for the Analytical Assessment of Aircraft Handling Qualities; I. Introduction and Background; II. Structural Model of the Human Pilot; III. Handling Qualities Metric; IV. Control Sensitivity; V. Applicability of the Methodology. | |
| 505 | 8 | |a VI. ConclusionsReferences; Chapter 6. Identification of Pilot-Vehicle Dynamics from Simulation and Flight Test; I. Introduction; II. Identification Techniques; III. Examples; IV. Conclusions; References; Chapter 7. Strapdown Inertial Navigation System Requirements Imposed by Synthetic Aperture Radar; I. Introduction; II. Background; III. Analysis for Straight and Level Mapping Segment; IV. Operation in the Presence of Acceleration; V. Modification to Permit Update/Alignment during a Frame; VI. Conclusions; Appendix A. Background for Synthetic Aperture Radar Degradation Analysis. | |
| 505 | 8 | |a Appendix B. Checklist of Issues to Be RaisedReferences; Chapter 8. Trajectory Estimation Algorithm Using Angles-Only, Multisensor Tracking Techniques; I. Introduction; II. Development of Triangulation Trajectory Tracker; III. Triangulation Trajectory Tracker Algorithm Performance; IV. Algorithm Performance Comparison; V. Conclusions; References; Chapter 9. A Perturbation Approach to the Maneuvering and Control of Space Structures; I. Introduction; II. Pseudomodal Equations of Motion; III. Control Strategy; IV. Control of the Elastic Model; V. Design of a Reduced-Order Compensator. | |
| 520 | |a Control and Dynamic Systems V33: Advances in Aerospace Systems Dynamics and Control Systems Part 3 of 3. | ||
| 546 | |a English. | ||
| 650 | 0 | |a Control theory. | |
| 650 | 0 | |a System analysis. | |
| 650 | 0 | |a Flight control. | |
| 650 | 2 | |a Systems Analysis |0 (DNLM)D013597 | |
| 650 | 6 | |a Th�eorie de la commande. |0 (CaQQLa)201-0012168 | |
| 650 | 6 | |a Analyse de syst�emes. |0 (CaQQLa)201-0007674 | |
| 650 | 6 | |a Syst�emes de commande (Vol) |0 (CaQQLa)201-0017045 | |
| 650 | 7 | |a systems analysis. |2 aat |0 (CStmoGRI)aat300077662 | |
| 650 | 7 | |a TECHNOLOGY & ENGINEERING |x Engineering (General) |2 bisacsh | |
| 650 | 7 | |a Control theory |2 fast |0 (OCoLC)fst00877085 | |
| 650 | 7 | |a Flight control |2 fast |0 (OCoLC)fst00927313 | |
| 650 | 7 | |a System analysis |2 fast |0 (OCoLC)fst01141385 | |
| 650 | 7 | |a AUTOMATIC CONTROL. |2 nasat | |
| 650 | 7 | |a CONTROL THEORY. |2 nasat | |
| 650 | 7 | |a CONTROL SYSTEMS DESIGN. |2 nasat | |
| 650 | 7 | |a DYNAMICAL SYSTEMS. |2 nasat | |
| 650 | 7 | |a SYSTEM IDENTIFICATION. |2 nasat | |
| 650 | 7 | |a SYNTHETIC APERTURES. |2 nasat | |
| 650 | 7 | |a ALGORITHMS. |2 nasat | |
| 650 | 7 | |a TRAJECTORY MEASUREMENT. |2 nasat | |
| 650 | 7 | |a EQUATIONS OF MOTION. |2 nasat | |
| 650 | 7 | |a AEROSPACE SYSTEMS. |2 nasat | |
| 650 | 7 | |a DYNAMIC CONTROL. |2 nasat | |
| 650 | 7 | |a ADAPTIVE CONTROL. |2 nasat | |
| 650 | 7 | |a DIGITAL FILTERS. |2 nasat | |
| 700 | 1 | |a Leondes, Cornelius T. | |
| 776 | 0 | 8 | |i Print version: |t Control and dynamic systems : Volume 33, Advances in aerospace systems dynamics and control systems. Part 3 of 3. |d San Diego : Academic Press, �1990 |z 0120127334 |w (OCoLC)21953076 |
| 830 | 0 | |a Control and dynamic systems ; |v v. 33. | |
| 856 | 4 | 0 | |u https://sciencedirect.uam.elogim.com/science/book/9780120127337 |z Texto completo |