Applied min-max approach to missile guidance and control:
Saved in:
| Main Author: | |
|---|---|
| Format: | Book |
| Language: | English |
| Published: |
Reston, Va.
American Institute of Aeronautics and Astronautics
2005
|
| Series: | Progress in astronautics and aeronautics
209 |
| Subjects: | |
| Online Access: | Table of contents Inhaltsverzeichnis |
| Item Description: | Includes bibliographical references and index |
| Physical Description: | XVII, 298 S. Ill., graph. Darst. 24 cm |
| ISBN: | 1563476959 9781563476952 |
Staff View
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Record in the Search Index
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| adam_text | APPLIED MIN-MAX APPROACH TO MISSILE GUIDANCE AND CONTROL SHAUL GUTMAN
FACULTY OF MECHANICAL ENGINEERING TECHNION, HAIFA, ISRAEL VOLUME 209
PROGRESS IN ASTRONAUTICS AND AERONAUTICS PAUL ZARCHAN, EDITOR-IN-CHIEF
MIT LINCOLN LABORATORY LEXINGTON, MASSACHUSETTS PUBLISHED BY THE
AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS, INC. 1801 ALEXANDER
BELL DRIVE, RESTON, VIRGINIA 20191-4344 TABLE OF CONTENTS PREFACE IX
ACKNOWLEDGMENTS XIII CHAPTER 1. DYNAMICAL SYSTEMS 1 I. INTRODUCTION 1 A.
DEFINITIONS 1 B. LAGRANGE EQUATIONS 1 C. ORDINARY AND GENERALIZED
DYNAMICAL SYSTEMS 2 D. LINEAR DYNAMICAL SYSTEMS 3 E. LYAPUNOV STABILITY
AND SYNTHESIS 17 F. OPTIMAL CONTROL AND DIFFERENTIAL GAMES 22 G.
NUMERICAL APPROACH 25 H. NOTES 27 REFERENCES 28 I. CONTROL OF UNCERTAIN
DYNAMICAL SYSTEMS CHAPTER 2. MODELING OF UNCERTAIN SYSTEMS 31 I.
INTRODUCTION 31 A. NATURE OF UNCERTAINTY 31 B. PARAMETER UNCERTAINTY IN
TIME-INVARIANT PLANTS. 32 C. UNMODELED DYNAMICS IN TIME-INVARIANT PLANTS
34 D. EXTERNAL DISTURBANCES 35 E. MATCHING CONDITIONS 37 F. UNSTRUCTURED
UNCERTAINTY 40 II. NOTES 41 REFERENCES 41 CHAPTER 3. STABILITY OF LINEAR
SYSTEMS AND ROOT CLUSTERING 43 I. INTRODUCTION 43 A. ASYMPTOTIC
STABILITY 43 B. RELATIVE STABILITY AND ROOT CLUSTERING 45 C. ROOT
CLUSTERING IN PARAMETER SPACE 54 D. ROBUST STABILITY 57 E. NOMINAL
CONTROL: MINIMIZING THE INTEGRAL SQUARE OF A SIGNAL 60 F. NOMINAL
CONTROL: STABILITY PERSPECTIVE 62 G. NOMINAL CONTROL: FULL ORDER 67 H.
SIMULTANEOUS STABILITY 69 II. NOTES 71 REFERENCES 72 XV XVI CHAPTER 4.
LINEAR MIN-MAX CONTROL OF UNCERTAIN CONSTANT PARAMETERS 75 I.
INTRODUCTION 75 A. FEEDBACK FORM 75 B. MIN-MAX PRINCIPLE 76 C. NECESSARY
CONDITIONS FOR MAX-MIN: LARGEST UNCERTAINTY POSSIBLE .. 79 D. GLOBAL
APPROACH 92 E. NECESSARY CONDITIONS FOR MAX-MIN: UNCERTAINTY REGION IS
GIVEN .. 112 F. COMPARISON WITH A FREQUENCY DOMAIN APPROACH: H 113 II.
NOTES 115 REFERENCES 115 CHAPTER 5. DISTURBANCE REJECTION 117 I.
INTRODUCTION 117 A. LINEAR DYNAMICS AND QUADRATIC COST 117 B.
DISTURBANCE REJECTION 119 C. POLYNOMIAL VERSION 121 D. DISTURBANCE
REJECTION IN THE PRESENCE OF REAL PARAMETER UNCERTAINTY 128 H. NOTES 129
REFERENCES 129 CHAPTER 6. MIN-MAX CONTROL FOR GENERAL PARAMETERS AND
INPUT DISTURBANCES 131 I. INTRODUCTION 131 A. MOTIVATION: INPUT
DISTURBANCE 131 B. SINGLE-VALUED DISCONTINUOUS CONTROL 135 C.
GENERALIZED DYNAMICAL SYSTEMS . .: 138 * D. STABILITY OF MATCHED
SYSTEMS 140 E. STABILITY OF MISMATCHED SYSTEMS 143 F. VARIABLE STRUCTURE
SYSTEMS 145 G. LINEAR CONTROL 150 H. QUADRATIC STABILIZABILITY 154 I.
NONLINEAR SYSTEMS IN THE PRESENCE OF REAL PARAMETER UNCERTAINTY .. 157
J. TRACKING 158 K. MECHANICAL MANIPULATORS 160 H NOTES 161 REFERENCES
161 II. OPTIMAL GUIDANCE FOR HOMING MISSILES CHAPTER 7. GUIDANCE SYSTEMS
165 I. INTRODUCTION 165 A. PROPORTIONAL NAVIGATION 165 B. GUIDANCE TO
COLLISION 166 C. LINEAR STATE MODEL: CONSTANT SPEED MISSILE 178 D.
LINEAR STATE MODEL: VARIABLE SPEED MISSILE 182 XVII E. THE GENERAL FORM:
ZERO EFFORT MISS 183 F. TARGET MODELING 190 II. NOTES 192 REFERENCES 192
CHAPTER 8. SIMPLE LINEAR DIFFERENTIAL GAMES 193 I. INTRODUCTION 193 A.
GAME FORMULATION 193 B. OPTIMAL STRATEGIES 194 C. SPECIAL CASES 198 D.
STATIONARY SYSTEMS 199 E. REMARKS ON TARGET ESTIMATION 200 N. NOTES 202
REFERENCES 203 CHAPTER 9. OPTIMAL GUIDANCE AND GUARANTEED MISS DISTANCE
205 I. INTRODUCTION 205 A. STATIONARY SYSTEMS WITH IDEAL TARGET 206 B.
FIRST-ORDER MODEL 210 C. NOSE VS TAIL CONTROL 218 D. GENERAL DYNAMICS:
NOSE CONTROL 219 E. SOME EXAMPLES 221 F. COMPARISON WITH OPTIMAL CONTROL
228 G. ACCELERATING MISSILE: THRUST EFFECT 237 H. ACCELERATING MISSILE:
FIRST-ORDER DYNAMICS 242 I. ACCELERATING MISSILE: HIGH-ORDER DYNAMICS
244 II. NOTES 247 REFERENCES .- 247 CHAPTER 10. CASESTUDIES 249 I.
INTRODUCTION 249 A. THRUST VECTOR CONTROL (TVC) *. 249 B. ANTIBALLISTIC
MISSILE: HIGH-ALTITUDE INTERCEPTION 269 C. ANTIBALLISTIC MISSILE:
ATMOSPHERIC INTERCEPTION 272 D. ANTIBALLISTIC MISSILE: BOOSTING TARGETS
273 II. NOTES 285 REFERENCES 285 EPILOGUE 287 INDEX 291 SUPPORTING
MATERIALS 299
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| spelling | Gutman, Shaul Verfasser aut Applied min-max approach to missile guidance and control Shaul Gutman Reston, Va. American Institute of Aeronautics and Astronautics 2005 XVII, 298 S. Ill., graph. Darst. 24 cm txt rdacontent n rdamedia nc rdacarrier Progress in astronautics and aeronautics 209 Includes bibliographical references and index Commande, Théorie de la Missiles - Commande, Systèmes de Missiles - Commande, Systèmes de - Modèles mathématiques Missiles - Guidage, Systèmes de Mathematisches Modell Guided missiles Guidance systems Control theory Guided missiles Control systems Mathematical models Guided missiles Control systems Robuste Regelung (DE-588)4206985-3 gnd rswk-swf Lenkflugkörper (DE-588)4035334-5 gnd rswk-swf Raketensteuerung (DE-588)4176902-8 gnd rswk-swf Flugregelung (DE-588)4328094-8 gnd rswk-swf Lenkflugkörper (DE-588)4035334-5 s Raketensteuerung (DE-588)4176902-8 s Flugregelung (DE-588)4328094-8 s Robuste Regelung (DE-588)4206985-3 s DE-604 Progress in astronautics and aeronautics 209 (DE-604)BV002331182 209 http://www.loc.gov/catdir/toc/fy0716/2007533417.html Table of contents GBV Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=017387922&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Gutman, Shaul Applied min-max approach to missile guidance and control Progress in astronautics and aeronautics Commande, Théorie de la Missiles - Commande, Systèmes de Missiles - Commande, Systèmes de - Modèles mathématiques Missiles - Guidage, Systèmes de Mathematisches Modell Guided missiles Guidance systems Control theory Guided missiles Control systems Mathematical models Guided missiles Control systems Robuste Regelung (DE-588)4206985-3 gnd Lenkflugkörper (DE-588)4035334-5 gnd Raketensteuerung (DE-588)4176902-8 gnd Flugregelung (DE-588)4328094-8 gnd |
| subject_GND | (DE-588)4206985-3 (DE-588)4035334-5 (DE-588)4176902-8 (DE-588)4328094-8 |
| title | Applied min-max approach to missile guidance and control |
| title_auth | Applied min-max approach to missile guidance and control |
| title_exact_search | Applied min-max approach to missile guidance and control |
| title_full | Applied min-max approach to missile guidance and control Shaul Gutman |
| title_fullStr | Applied min-max approach to missile guidance and control Shaul Gutman |
| title_full_unstemmed | Applied min-max approach to missile guidance and control Shaul Gutman |
| title_short | Applied min-max approach to missile guidance and control |
| title_sort | applied min max approach to missile guidance and control |
| topic | Commande, Théorie de la Missiles - Commande, Systèmes de Missiles - Commande, Systèmes de - Modèles mathématiques Missiles - Guidage, Systèmes de Mathematisches Modell Guided missiles Guidance systems Control theory Guided missiles Control systems Mathematical models Guided missiles Control systems Robuste Regelung (DE-588)4206985-3 gnd Lenkflugkörper (DE-588)4035334-5 gnd Raketensteuerung (DE-588)4176902-8 gnd Flugregelung (DE-588)4328094-8 gnd |
| topic_facet | Commande, Théorie de la Missiles - Commande, Systèmes de Missiles - Commande, Systèmes de - Modèles mathématiques Missiles - Guidage, Systèmes de Mathematisches Modell Guided missiles Guidance systems Control theory Guided missiles Control systems Mathematical models Guided missiles Control systems Robuste Regelung Lenkflugkörper Raketensteuerung Flugregelung |
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