Computational space flight mechanics:
Saved in:
| Main Author: | |
|---|---|
| Format: | Book |
| Language: | English |
| Published: |
Berlin ; Heidelberg
Springer
2010
|
| Subjects: | |
| Online Access: | Inhaltstext Inhaltsverzeichnis |
| Item Description: | Zusätzliches Online-Angebot unter www.://extra.springer.com. - Literaturangaben |
| Physical Description: | XIII, 300 S. graph. Darst. 24 cm |
| ISBN: | 9783642135828 |
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Record in the Search Index
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| adam_text |
IMAGE 1
TABLE OF CONTENTS
1 INTRODUCTION 1
REFERENCES 4
2 COORDINATE TRANSFORMATIONS 7
2.1 BASIC ROTATIONAL TRANSFORMATIONS 8
2.2 TIME DERIVATIVE OF VECTORS IN MOVING FRAMES 11
2.2.1 THE VELOCITY VECTOR 11
2.2.2 THE ACCELERATION VECTOR 14
2.3 THE ANGULAR VELOCITY IN A BODY FRAME: EULER ANGLES 17 2.4 PROBLEMS
22
REFERENCES 23
3 TRANSFORMATIONS BETWEEN OFTEN USED COORDINATE SYSTEMS 25
3. 1 TRANSFORMATION FROM GEODETIC TO BODY FRAME 25
3.2 TRANSFORMATION FROM AIR PATH TO BODY FRAME 26
3.3 TRANSFORMATION FROM GEODETIC TO FLIGHT PATH FRAME 27 3.4
TRANSFORMATION FROM PLANETOCENTRIC TO ORBITAL FRAME 28 3.5 PROBLEMS 30
REFERENCES 31
4 KEPLER'S LAWS OF PLANETARY MOTION AND NEWTON'S CELESTIAL MECHANICS 33
4.1 KEPLER'S 1. LAW 33
4.2 KEPLER'S 2. LAW 34
4.3 KEPLER'S 3. LAW 36
4.4 NEWTON'S CELESTIAL MECHANICS 37
4.5 PROBLEMS 42
REFERENCES 43
5 THE TWO-BODY PROBLEM 45
5.1 THE EQUATION OF MOTION 45
5.2 THE ENERGY CONSERVATION 47
BIBLIOGRAFISCHE INFORMATIONEN HTTP://D-NB.INFO/1002539994
DIGITALISIERT DURCH
IMAGE 2
X TABLE OF CONTENTS
5.3 THE ANGULAR MOMENTUM CONSERVATION 48
5.4 THE ORBIT EQUATION 49
5.5 THE VARIOUS ORBITS 51
5.5.1 THE ECCENTRICITY E 1 51
5.5.2 THE ECCENTRICITY E 1 53
5.6 TEST CASES FOR THE THREE CLASSES OF ORBITS 54
5.7 TIME DEPENDENCY OF THE ORBITAL VARIABLES R AND 6 AND KEPLER'S
EQUATION 56
5.7.1 THE ELLIPTICAL ORBIT 59
5.7.2 SOLUTIONS OF THE ELLIPTICAL TEST CASE 1 62
5.7.3 THE HYPERBOLIC ORBIT 64
5.7.4 SOLUTIONS OF THE HYPERBOLIC TEST CASE 3 66
5.8 THE CLASSICAL ORBITAL ELEMENTS 67
5.8.1 DERIVATION OF RELATIONS 67
5.8.2 SAMPLE CALCULATIONS OF TEST CASE 1 USING ORBITAL ELEMENTS 71
5.8.3 SAMPLE CALCULATIONS OF TEST CASE 1 USING THE GENERAL EQUATIONS OF
PLANETARY FLIGHT 73
5.9 PERTURBATIONS OF ORBITAL DYNAMICS 75
5.9.1 LAGRANGE'S PLANET EQUATIONS 76
5.9.2 NUMERICAL SOLUTIONS OF LAGRANGE'S PLANET EQUATIONS 80
5.9.3 NUMERICAL SOLUTION OF THE GENERAL EQUATIONS OF PLANETARY FLIGHT
FOR AN ASPHERICAL EARTH 87
5.10 PROBLEMS 91
REFERENCES 92
6 GENERAL EQUATIONS FOR PLANETARY FLIGHT 93
6.1 EQUATIONS OF TRANSLATIONAL MOTION 93
6.1.1 FLIGHT WITHOUT BANK ANGLE 93
6.1.2 FLIGHT WITH BANK ANGLE 101
6.1.3 EQUATIONS INCLUDING SIDE FORCES 103
6.1.4 FLIGHT WITH PROPULSION FORCE 105
6.1.5 ORBITAL FLIGHT AROUND AN ASPHERICAL EARTH 106
6.2 EQUATIONS OF ROTATIONAL MOTION 109
6.3 SET OF EQUATIONS FOR SIX DEGREE OF FREEDOM SIMULATIONS 114 6.4
PROBLEMS 118
REFERENCES 119
7 A RESUME OF THE AEROTHERMODYNAMICS OF SPACE FLIGHT VEHICLES 121
7.1 CONVENTIONS FOR AEROTHERMODYNAMIC DATA 121
7.2 FLOW REGIMES AND PHYSICAL PHENOMENA 123
IMAGE 3
TABLE OF CONTENTS XI
7.3 AEROTHERMODYNAMIC DATA OF THE X-38 VEHICLE 126
7.3.1 DATA OF LONGITUDINAL MOTION 128
7.3.2 DATA OF LATERAL MOTION 132
7.4 PROBLEMS 135
REFERENCES 135
8 THREE AND SIX DEGREE OF FREEDOM TRAJECTORY SIMULATIONS 137
8.1 THREE DEGREE OF FREEDOM SIMULATION FOR A WINGED SPACE VEHICLE 137
8.2 THREE DEGREE OF FREEDOM SIMULATION FOR A NON-WINGED SPACE VEHICLE
141
8.3 SIX DEGREE OF FREEDOM SIMULATIONS FOR A WINGED SPACE VEHICLE 145
8.3.1 FLIGHT WITH STATICALLY STABLE LONGITUDINAL MOTION . . . 145 8.3.2
FLIGHT WITH STATICALLY STABLE LONGITUDINAL AND YAW MOTION 150
8.4 PROBLEMS 152
REFERENCES 152
9 NUMERICAL APPLICATIONS OF THE GENERAL EQUATIONS FOR PLANETARY FLIGHT
153
9.1 FLIGHT IN GEOSTATIONARY ORBIT 154
9.2 FLIGHT IN LOW EARTH ORBIT 156
9.2.1 CIRCULAR EQUATORIAL ORBIT (INCLINATION ANGLE J = 0 ) . . 156
9.2.2 CIRCULAR ORBIT WITH INCLINATION ANGLE 4 ^ 0 158
9.3 ELLIPTICAL ORBITS 160
9.3.1 ELLIPTICAL ORBIT WITHOUT AERODYNAMIC FORCES 162 9.3.2 ELLIPTICAL
ORBIT WITH AERODYNAMIC FORCES 167
9.3.3 ELLIPTICAL ORBITS WITH FLIGHT IN OTHER DIRECTIONS THAN WEST-EAST
172
9.4 RE-ENTRY FLIGHT 174
9.4.1 DECELERATION OF SPACE VEHICLES AND G-LOADS 180 9.5 PLANETARY
FLIGHT AND AEROCAPTURING MISSION 186
9.6 ARTILLERY BALLISTICS 193
9.6.1 PROJECTILE'S FLIGHT WITHOUT AERODYNAMIC DRAG 193 9.6.2
PROJECTILE'S FLIGHT WITH AERODYNAMIC DRAG 195
9.6.3 THE PRINCIPLE EQUATION OF BALLISTICS 199
9.6.4 APPROXIMATE SOLUTIONS OF THE PRINCIPLE EQUATION OF BALLISTICS 203
9.6.5 SHOTS OF SHELLS TOWARDS THE FOUR CARDINAL POINTS 206 9.7 ANOTHER
ILLUSTRATING CASE 208
9.8 CONCLUSION 212
9.9 PROBLEMS 213
REFERENCES 214
IMAGE 4
XII TABLE OF CONTENTS
10 THE EARTH ATMOSPHERE 215
REFERENCES 221
11 SOLUTION OF PROBLEMS 223
11.1 PROBLEMS OF CHAPTER 2 223
11.2 PROBLEMS OF CHAPTER 3 224
11.3 PROBLEMS OF CHAPTER 4 225
11.4 PROBLEMS OF CHAPTER 5 228
11.5 PROBLEMS OF CHAPTER 6 229
11.6 PROBLEMS OF CHAPTER 7 231
11.7 PROBLEMS OF CHAPTER 8 232
11.8 PROBLEMS OF CHAPTER 9 232
REFERENCE 233
APPENDIX A OUR PLANETARY SYSTEM 235
A.I THE FIRST FOUR PLANETS IN THE SOLAR SYSTEM 235
A.2 THE FIRST SIX PLANETS IN THE SOLAR SYSTEM 236
A.3 THE ENTIRE SOLAR SYSTEM 237
REFERENCES 238
APPENDIX B FORTRAN CODES 239
B.I GENERAL EQUATIONS FOR PLANETARY FLIGHT - THREE DEGREE OF FREEDOM
SIMULATION 239
B.2 ORBIT DETERMINATION WITH ORBITAL ELEMENTS 245
B.3 LAGRANGE'S PLANET EQUATIONS 250
REFERENCES 259
APPENDIX C MATLAB CODES 261
C.I KEPLER'S EQUATION FOR ELLIPTICAL ORBITS 261
C.2 AREA APPROACH FOR ELLIPTICAL ORBITS 263
C.3 AREA APPROACH FOR HYPERBOLIC ORBITS 266
C.4 SIX DEGREE OF FREEDOM SIMULATION 268
REFERENCES 282
A P P E N D IX D C O N S T A N T S, R E L A T I O N S, U N I TS A ND C O
N V E R S I O NS . . . 283
D.I CONSTANTS AND RELATIONS 283
D.2 UNITS AND CONVERSIONS 284
REFERENCES 286
APPENDIX E SYMBOLS 287
E.I LATIN LETTERS 287
E.2 GREEK LETTERS 290
E.3 INDICES 291
E.3.1 UPPER INDICES 291
E.3.2 LOWER INDICES 291
E.4 OTHER SYMBOLS 292
IMAGE 5
TABLE OF CONTENTS XIII
APPENDIX F GLOSSARY, ABBREVIATIONS, ACRONYMS 293 F.I GLOSSARY 293
F.2 ABBREVIATIONS, ACRONYMS 294
NAME INDEX 295
SUBJECT INDEX 297 |
| any_adam_object | 1 |
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| dewey-ones | 629 - Other branches of engineering |
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| dewey-search | 629.4 |
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| dewey-tens | 620 - Engineering and allied operations |
| discipline | Maschinenbau / Maschinenwesen Verkehr / Transport |
| format | Book |
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| spelling | Weiland, Claus Verfasser aut Computational space flight mechanics Claus Weiland Berlin ; Heidelberg Springer 2010 XIII, 300 S. graph. Darst. 24 cm txt rdacontent n rdamedia nc rdacarrier Zusätzliches Online-Angebot unter www.://extra.springer.com. - Literaturangaben Flugmechanik (DE-588)4154760-3 gnd rswk-swf Raumflugkörper (DE-588)4177066-3 gnd rswk-swf Numerisches Verfahren (DE-588)4128130-5 gnd rswk-swf Raumflugkörper (DE-588)4177066-3 s Flugmechanik (DE-588)4154760-3 s Numerisches Verfahren (DE-588)4128130-5 s DE-604 X:MVB text/html http://deposit.dnb.de/cgi-bin/dokserv?id=3476708&prov=M&dok_var=1&dok_ext=htm Inhaltstext DNB Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=021143894&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
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| title | Computational space flight mechanics |
| title_auth | Computational space flight mechanics |
| title_exact_search | Computational space flight mechanics |
| title_full | Computational space flight mechanics Claus Weiland |
| title_fullStr | Computational space flight mechanics Claus Weiland |
| title_full_unstemmed | Computational space flight mechanics Claus Weiland |
| title_short | Computational space flight mechanics |
| title_sort | computational space flight mechanics |
| topic | Flugmechanik (DE-588)4154760-3 gnd Raumflugkörper (DE-588)4177066-3 gnd Numerisches Verfahren (DE-588)4128130-5 gnd |
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