Advances in missile guidance theory:
Gespeichert in:
| Hauptverfasser: | , |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Reston, Va.
AIAA
1998
|
| Schriftenreihe: | Progress in astronautics and aeronautics
180 |
| Schlagworte: | |
| Online-Zugang: | Inhaltsverzeichnis |
| Beschreibung: | Diskette u.d.T.: Advances in missile guidance theory software Version 1.0. - Systemvoraussetzungen: IBM compatible |
| Beschreibung: | X, 200 S. graph. Darst. 1 Diskette (9 cm) |
| ISBN: | 1563472759 |
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Datensatz im Suchindex
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| adam_text | ADVANCES IN MISSILE GUIDANCE THEORY JOSEPH Z. BEN-ASHER AND ISAAC YAESH
ISRAEL MILITARY INDUSTRIES*ADVANCED SYSTEMS DIVISION RAMAT-HA SHARON,
ISRAEL VOLUME 180 PROGRESS IN ASTRONAUTICS AND AERONAUTICS PAUL ZARCHAN,
EDITOR-IN-CHIEF CHARLES STARK DRAPER LABORATORY, INC. CAMBRIDGE,
MASSACHUSETTS PUBLISHED BY THE AMERICAN INSTITUTE OF AERONAUTICS AND
ASTRONAUTICS, INC. 1801 ALEXANDER BELL DRIVE, RESTON, VIRGINIA
20191-4344 TABLE OF CONTENTS PREFACE VII CHAPTER 1. INTRODUCTION 1 I.
OBJECTIVES AND MOTIVATION 1 II. HISTORICAL BACKGROUND 1 III.
MATHEMATICAL MODELING 3 REFERENCES 6 CHAPTER 2. MATHEMATICAL BACKGROUND
7 I. SCOPE AND PRELIMINARIES 7 II. GAME RULES SPECIFICATIONS 9 III.
CANDIDATES FOR SADDLE-POINT SOLUTIONS 10 IV. RICCATI EQUATION 13 V.
SUFFICIENT CONDITION 15 VI. ADJOINT ANALYSIS 17 VII. SUMMARY AND
CONCLUSIONS 22 REFERENCES ,23 CHAPTER 3. OPTIMAL GUIDANCE BASED ON
LINEAR-QUADRATIC ONE-SIDED OPTIMIZATION 25 I. INTRODUCTION . . . 25 II.
PROBLEM FORMULATION 25 IN. NONMANEUVERING TARGET 26 IV. MANEUVERING
TARGET 32 V. MATLAB* SIMULATIONS 43 VI. NUMERICAL EXAMPLES 55 VII.
CONCLUDING REMARKS I 87 REFERENCES 88 CHAPTER 4. OPTIMAL GUIDANCE BASED
ON LINEAR-QUADRATIC DIFFERENTIAL GAMES 89 I. INTRODUCTION 89 N. IDEAL
PURSUER CASE . . . 89 IN. NONIDEAL PURSUER CASE . . 95 IV. ADDING A
CONSTANT MANEUVER TO THE PURSUIT-EVASION PROBLEM . . . 102 V. GENERAL
SOLUTION FOR IDEAL ADVERSARIES 105 VI. NUMERICAL EXAMPLES 107 VII.
CONCLUSIONS 125 REFERENCES 126 CHAPTER 5. OPTIMAL GUIDANCE WITH REDUCED
SENSITIVITY TO TIME-TO-GO ESTIMATION ERRORS 127 I. INTRODUCTION 127 VII
VIII II. PROBLEM FORMULATION 128 III. OPTIMAL FEEDBACK SOLUTION 129 IV.
MATLAB SIMULATION 131 V. NUMERICAL RESULTS 131 VI. CONCLUSIONS 139
REFERENCES 140 CHAPTER 6. ROBUST GUIDANCE METHODS 141 I. INTRODUCTION
141 II. THE PROBLEM OF UNCERTAIN T 141 HI. THE AUXILIARY PROBLEM 143 IV.
MATLAB SIMULATION 147 V. NUMERICAL EXAMPLE 148 VI. CONCLUSIONS 154
REFERENCES 157 CHAPTER 7. OPTIMAL GUIDANCE WITH MULTIPLE TARGETS 159 I.
INTRODUCTION 159 II. TERMINAL AND INTERIOR POINT CONSTRAINTS 159 HI.
PROBLEM FORMULATION 160 IV. OPTIMAL SOLUTION 160 V. SPECIAL CASES 164
VI. NUMERICAL EXAMPLE 166 VII. CONCLUSIONS : . . . 169 REFERENCES 169
APPENDIX A JUSTIFICATION OF THE SWEEP ASSUMPTION 171 APPENDIX B
MATHEMATICAL COMPUTATIONS WITH MAPLE 175 I. GENERAL . 175 II. PROGRAM
DESCRIPTION AND ITS USE IN LLIIS BOOK 175 III. ASSIGNING AND UNASSIGNING
VARIABLES 175 IV. EVALUATING EXPRESSIONS 176 V. SOLVING EQUATIONS * 176
VI. LINEAR ALGEBRA 177 VII. REPRESENTATIVE EXAMPLES 178 VIII. CONCLUDING
REMARKS 179 REFERENCES 179 APPENDIX C NUMERICAL COMPUTATIONS WITH MATLAB
181 I. SCOPE 181 II. BRIEF INTRODUCTION TO MATLAB 181 III.
DEMONSTRATIVE EXAMPLE 184 IV. USAGE OF THE MATLAB PROGRAMS 186 V.
CONCLUDING REMARKS 186 REFERENCE 186 INDEX 187
|
| adam_txt |
ADVANCES IN MISSILE GUIDANCE THEORY JOSEPH Z. BEN-ASHER AND ISAAC YAESH
ISRAEL MILITARY INDUSTRIES*ADVANCED SYSTEMS DIVISION RAMAT-HA'SHARON,
ISRAEL VOLUME 180 PROGRESS IN ASTRONAUTICS AND AERONAUTICS PAUL ZARCHAN,
EDITOR-IN-CHIEF CHARLES STARK DRAPER LABORATORY, INC. CAMBRIDGE,
MASSACHUSETTS PUBLISHED BY THE AMERICAN INSTITUTE OF AERONAUTICS AND
ASTRONAUTICS, INC. 1801 ALEXANDER BELL DRIVE, RESTON, VIRGINIA
20191-4344 TABLE OF CONTENTS PREFACE VII CHAPTER 1. INTRODUCTION 1 I.
OBJECTIVES AND MOTIVATION 1 II. HISTORICAL BACKGROUND 1 III.
MATHEMATICAL MODELING 3 REFERENCES 6 CHAPTER 2. MATHEMATICAL BACKGROUND
7 I. SCOPE AND PRELIMINARIES 7 II. GAME RULES SPECIFICATIONS 9 III.
CANDIDATES FOR SADDLE-POINT SOLUTIONS 10 IV. RICCATI EQUATION 13 V.
SUFFICIENT CONDITION 15 VI. ADJOINT ANALYSIS 17 VII. SUMMARY AND
CONCLUSIONS 22 REFERENCES ,23 CHAPTER 3. OPTIMAL GUIDANCE BASED ON
LINEAR-QUADRATIC ONE-SIDED OPTIMIZATION 25 I. INTRODUCTION . . . 25 II.
PROBLEM FORMULATION 25 IN. NONMANEUVERING TARGET 26 IV. MANEUVERING
TARGET 32 V. MATLAB* SIMULATIONS 43 VI. NUMERICAL EXAMPLES 55 VII.
CONCLUDING REMARKS I 87 REFERENCES 88 CHAPTER 4. OPTIMAL GUIDANCE BASED
ON LINEAR-QUADRATIC DIFFERENTIAL GAMES 89 I. INTRODUCTION 89 N. IDEAL
PURSUER CASE . . . 89 IN. NONIDEAL PURSUER CASE . . 95 IV. ADDING A
CONSTANT MANEUVER TO THE PURSUIT-EVASION PROBLEM . . . 102 V. GENERAL
SOLUTION FOR IDEAL ADVERSARIES 105 VI. NUMERICAL EXAMPLES 107 VII.
CONCLUSIONS 125 REFERENCES 126 CHAPTER 5. OPTIMAL GUIDANCE WITH REDUCED
SENSITIVITY TO TIME-TO-GO ESTIMATION ERRORS 127 I. INTRODUCTION 127 VII
VIII II. PROBLEM FORMULATION 128 III. OPTIMAL FEEDBACK SOLUTION 129 IV.
MATLAB SIMULATION 131 V. NUMERICAL RESULTS 131 VI. CONCLUSIONS 139
REFERENCES 140 CHAPTER 6. ROBUST GUIDANCE METHODS 141 I. INTRODUCTION
141 II. THE PROBLEM OF UNCERTAIN T 141 HI. THE AUXILIARY PROBLEM 143 IV.
MATLAB SIMULATION 147 V. NUMERICAL EXAMPLE 148 VI. CONCLUSIONS 154
REFERENCES 157 CHAPTER 7. OPTIMAL GUIDANCE WITH MULTIPLE TARGETS 159 I.
INTRODUCTION 159 II. TERMINAL AND INTERIOR POINT CONSTRAINTS 159 HI.
PROBLEM FORMULATION 160 IV. OPTIMAL SOLUTION 160 V. SPECIAL CASES 164
VI. NUMERICAL EXAMPLE 166 VII. CONCLUSIONS : . . . 169 REFERENCES 169
APPENDIX A JUSTIFICATION OF THE SWEEP ASSUMPTION 171 APPENDIX B
MATHEMATICAL COMPUTATIONS WITH MAPLE 175 I. GENERAL ". 175 II. PROGRAM
DESCRIPTION AND ITS USE IN LLIIS BOOK 175 III. ASSIGNING AND UNASSIGNING
VARIABLES 175 IV. EVALUATING EXPRESSIONS 176 V. SOLVING EQUATIONS * 176
VI. LINEAR ALGEBRA 177 VII. REPRESENTATIVE EXAMPLES 178 VIII. CONCLUDING
REMARKS 179 REFERENCES 179 APPENDIX C NUMERICAL COMPUTATIONS WITH MATLAB
' 181 I. SCOPE 181 II. BRIEF INTRODUCTION TO MATLAB 181 III.
DEMONSTRATIVE EXAMPLE 184 IV. USAGE OF THE MATLAB PROGRAMS 186 V.
CONCLUDING REMARKS 186 REFERENCE 186 INDEX 187 |
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| illustrated | Illustrated |
| index_date | 2024-07-02T16:19:52Z |
| indexdate | 2024-07-09T20:51:44Z |
| institution | BVB |
| isbn | 1563472759 |
| language | English |
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| series | Progress in astronautics and aeronautics |
| series2 | Progress in astronautics and aeronautics |
| spelling | Ben-Asher, Joseph Z. Verfasser aut Advances in missile guidance theory Joseph Z. Ben-Asher and Isaac Yaesh Advances in missile guidance theory software Version 1.0 Reston, Va. AIAA 1998 X, 200 S. graph. Darst. 1 Diskette (9 cm) txt rdacontent n rdamedia nc rdacarrier Progress in astronautics and aeronautics 180 Diskette u.d.T.: Advances in missile guidance theory software Version 1.0. - Systemvoraussetzungen: IBM compatible Missiles - Guidage, Systèmes de Missiles balistiques - Guidance, Système de Ballistic missiles Guidance systems Guided missiles Guidance systems Flugregelung (DE-588)4328094-8 gnd rswk-swf Lenkflugkörper (DE-588)4035334-5 gnd rswk-swf Lenkflugkörper (DE-588)4035334-5 s Flugregelung (DE-588)4328094-8 s DE-604 Yaesh, Isaac Verfasser aut Progress in astronautics and aeronautics 180 (DE-604)BV001890233 180 GBV Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=015385296&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Ben-Asher, Joseph Z. Yaesh, Isaac Advances in missile guidance theory Progress in astronautics and aeronautics Missiles - Guidage, Systèmes de Missiles balistiques - Guidance, Système de Ballistic missiles Guidance systems Guided missiles Guidance systems Flugregelung (DE-588)4328094-8 gnd Lenkflugkörper (DE-588)4035334-5 gnd |
| subject_GND | (DE-588)4328094-8 (DE-588)4035334-5 |
| title | Advances in missile guidance theory |
| title_alt | Advances in missile guidance theory software Version 1.0 |
| title_auth | Advances in missile guidance theory |
| title_exact_search | Advances in missile guidance theory |
| title_exact_search_txtP | Advances in missile guidance theory |
| title_full | Advances in missile guidance theory Joseph Z. Ben-Asher and Isaac Yaesh |
| title_fullStr | Advances in missile guidance theory Joseph Z. Ben-Asher and Isaac Yaesh |
| title_full_unstemmed | Advances in missile guidance theory Joseph Z. Ben-Asher and Isaac Yaesh |
| title_short | Advances in missile guidance theory |
| title_sort | advances in missile guidance theory |
| topic | Missiles - Guidage, Systèmes de Missiles balistiques - Guidance, Système de Ballistic missiles Guidance systems Guided missiles Guidance systems Flugregelung (DE-588)4328094-8 gnd Lenkflugkörper (DE-588)4035334-5 gnd |
| topic_facet | Missiles - Guidage, Systèmes de Missiles balistiques - Guidance, Système de Ballistic missiles Guidance systems Guided missiles Guidance systems Flugregelung Lenkflugkörper |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=015385296&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
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