Fundamentals of astrodynamics and applications:
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Hawthorne, Calif.
Microcosm Press [u.a.]
2007
|
| Ausgabe: | 3. ed. |
| Schriftenreihe: | Space technology library
21 |
| Schlagworte: | |
| Online-Zugang: | Inhaltsverzeichnis |
| Beschreibung: | XXI, 1055 S. graph. Darst. |
| ISBN: | 9780387718316 9781881883142 |
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| 245 | 1 | 0 | |a Fundamentals of astrodynamics and applications |c David A. Vallado |
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Datensatz im Suchindex
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FUNDAMENTALS OF ASTRODYNAMICS AND APPLICATIONS THIRD EDITION DAVID A.
VALLADO WITH TECHNICAL CONTRIBUTIONS BY WAYNE D. MCCLAIN SPACE
TECHNOLOGY LIBRARY PUBLISHED JOINTLY BY MICROCOSM PRESS HAWTHORNE, CA
SPRINGER NEW YORK, NY TABLE OF CONTENTS VLL CHAPTER 1 EQUATIONS OF
MOTION 1.1 CHAPTER 2 CHAPTER 3 1.2 1.3 HISTORY .1.1 ANCIENT ERA . 1.2
THE COPERNICAN REVOLUTION .1.3 KEPLER'S LAWS .1.4 NEWTON'S LAWS .1.5
OTHER EARLY ASTRODYNAMIC CONTRIBUTIONS GEOMETRY OF CONIC SECTIONS .2.1
BASIC PARAMETERS TWO-BODY EQUATION .3.1 ASSUMPTIONS FOR THE TWO-BODY
EQUATION .3.2 SPECIFIC ANGULAR MOMENTUM .3.3 SPECIFIC MECHANICAL ENERGY
.3.4 KEPLER'S FIRST LAW (TRAJECTORY EQUATION) .3.5 KEPLER'S SECOND AND
THIRD LAWS .3.6 VELOCITY FORMULAS 1.4 THREE-BODY AND -BODY EQUATIONS
1.4.1 INERTIAL, RELATIVE, AND BARYCENTRIC FORMULAS 1.4.2 TEN KNOWN
INTEGRALS 1.4.3 GENERAL THREE-BODY PROBLEM KEPLER'S EQUATION AND
KEPLER'S PROBLEM 2.1 HISTORICAL BACKGROUND 2.2 KEPLER'S EQUATION 2.2.1
ALTERNATE FORMULATION FOR ECCENTRIC ANOMALY 2.2.2 FORMULATION FOR THE
PARABOLIC ANOMALY 2.2.3 FORMULATION FOR THE HYPERBOLIC ANOMALY 2.2.4
UNIVERSAL FORMULATION 2.2.5 SOLUTIONS OF KEPLER'S EQUATION 2.2.6 SUMMARY
AND RELATED FORMULAS 2.3 KEPLER'S PROBLEM 2.3.1 SOLUTION TECHNIQUES 2.4
SATELLITE STATE REPRESENTATIONS 2.4.1 CLASSICAL ORBITAL ELEMENTS
(KEPLERIAN) 2.4.2 TWO-LINE ELEMENT SETS 2.4.3 OTHER ELEMENT SETS 2.4.4
CANONICAL ELEMENTS 2.5 APPLICATION: ORBITAL ELEMENTS FROM R AND V 2.6
APPLICATION: R AND V FROM ORBITAL ELEMENTS 2.7 APPLICATION: GROUNDTRACKS
2.8 APPLICATION: FIND TIME OF FLIGHT (FINDTOF) COORDINATE AND TIME
SYSTEMS 3.1 HISTORICAL BACKGROUND 3.2 THE EARTH 3.2.1 LOCATION
PARAMETERS 3.2.2 SHAPE OF THE EARTH 3.2.3 GRAVITATIONAL MODEL 1 1 7 9 10
12 12 12 20 23 23 25 27 29 32 33 33 37 40 49 49 51 57 58 60 66 71 85 87
88 103 104 113 116 118 119 124 128 131 137 137 139 141 142 149 VLLL 3.3
COORDINATE SYSTEMS 153 3.3.1 INTERPLANETARY SYSTEMS 158 3.3.2
EARTH-BASED SYSTEMS 159 3.3.3 SATELLITE-BASED SYSTEMS 162 3.4 COORDINATE
TRANSFORMATIONS 166 3.4.1 COORDINATE ROTATION 167 3.4.2 ROTATING
TRANSFORMATIONS 173 3.4.3 COMMON TRANSFORMATIONS 174 3.4.4 APPLICATION:
CONVERTING UK (ECEF) TO LATITUDE AND LONGITUDE 176 3.5 TIME 181 3.5.1
SOLAR TIME AND UNIVERSAL TIME 184 3.5.2 SIDEREAL TIME 191 3.5.3 ATOMIC
TIME 196 3.5.4 DYNAMICAL TIME 197 3.5.5 COORDINATE TIME 200 3.5.6
CONVERSIONS 201 3.6 TIME CONVERSIONS 203 3.6.1 DMS TO RAD / RAD TO DMS
203 3.6.2 HMS TO RAD / RAD TO HMS 204 3.6.3
HMSTOTIMEOFDAY/TIMEOFDAYTOHMS 205 3.6.4 YMD TO DAY OF YEAR/DAY OF YEAR
TO YMD 206 3.6.5 YMDHMSTODAYS/DAYSTOYMDHMS 207 3.6.6 JULIAN DATE TO
GREGORIAN DATE 208 3.7 TRANSFORMING CELESTIAL AND TERRESTRIAL
COORDINATES 209 3.7.1 IAU-2000 RESOLUTIONS 217 3.7.2 VELOCITY
TRANSFORMATIONS 227 3.7.3 IAU-76 / FK5 REDUCTION 228 3.7.4 OTHER
REDUCTIONS 236 3.7.5 COMPUTATIONAL CONSIDERATIONS 240 3.8 EARTH MODELS
AND CONSTANTS 242 3.8.1 CANONICAL UNITS 242 CHAPTER 4 OBSERVATIONS 247
4.1 INTRODUCTION 247 4.2 OBTAINING DATA 248 4.2.1 QUANTITY OF DATA : 251
4.2.2 TYPES OF DATA 252 4.2.3 EXAMPLE APPLICATIONS 253 4.3 INTRODUCTION
TO SENSOR SYSTEMS 254 4.4 OBSERVATION TRANSFORMATIONS 258 4.4.1
GEOCENTRIC RIGHT ASCENSION AND DECLINATION 260 4.4.2 TOPOCENTRIC RIGHT
ASCENSION AND DECLINATION 263 4.4.3 AZIMUTH-ELEVATION 265 4.4.4
PRACTICAL AZ-EL CONVERSIONS 270 4.4.5 TRANSFORMATIONS FOR ECLIPTIC
LATITUDE AND LONGITUDE 272 4.4.6 PRACTICAL ASPECTS OF SURVEILLANCE 274
CHAPTER 5 CELESTIAL PHENOMENA 279 5.1 SOLAR PHENOMENA 279 5.1.1
APPLICATION: SUN POSITION VECTOR 279 5.1.2 APPLICATION: SUNRISE, SUNSET,
AND TWILIGHT TIMES 283 IX 5.2 LUNAR PHENOMENA 287 5.2.1 APPLICATION:
MOON POSITION VECTOR 288 5.2.2 APPLICATION: MOON RISE AND SET TIMES 292
5.2.3 PHASES OF THE MOON 296 5.3 CELESTIAL APPLICATIONS 296 5.3.1
APPLICATION: PLANETARY EPHEMERIDES 297 5.3.2 ECLIPSES 300 5.3.3
APPLICATION: SIGHT AND LIGHT 307 5.3.4 GROUND ILLUMINATION 311 5.3.5
MISCELLANEOUS PHENOMENA 313 CHAPTER 6 ORBITAL MANEUVERING 319 6.1
HISTORICAL BACKGROUND 319 6.2 INTRODUCTION 320 6.3 COPLANAR MANEUVERS
322 6.3.1 HOHMANN AND BI-ELLIPTIC TRANSFERS 324 6.3.2 COMPARING HOHMANN
AND BI-ELLIPTIC TRANSFERS 330 6.3.3 TRANSFERS USING THE ONE-TANGENT BURN
333 6.3.4 GENERAL TRANSFERS 339 6.4 NONCOPLANAR TRANSFERS 339 6.4.1
INTRODUCTION 339 6.4.2 INCLINATION-ONLY CHANGES 344 6.4.3 CHANGES IN THE
RIGHT ASCENSION OF THE ASCENDING NODE 347 6.4.4 CHANGES TO INCLINATION
AND THE ASCENDING NODE 350 6.5 COMBINED MANEUVERS 352 6.5.1
MINIMUM-INCLINATION MANEUVERS 353 6.5.2 FIXED-AL? MANEUVERING 356 6.6
CIRCULAR RENDEZVOUS 360 6.6.1 CIRCULAR COPLANAR PHASING 360 6.6.2
CIRCULAR NONCOPLANAR PHASING 367 6.7 CONTINUOUS-THRUST TRANSFERS . 373
6.7.1 INTRODUCTION 374 6.7.2 ORBIT RAISING 377 6.7.3 LOW-THRUST,
NONCOPLANAR TRANSFERS 383 6.8 RELATIVE MOTION 389 6.8.1 POSITION
SOLUTIONS FOR NEARLY CIRCULAR ORBITS 394 6.8.2 TREND ANALYSIS 398 6.8.3
ACCURACY ANALYSIS 412 CHAPTER 7 INITIAL ORBIT DETERMINATION 419 7.1
HISTORICAL BACKGROUND 419 7.2 OBSERVATIONS OF RANGE, AZIMUTH, AND
ELEVATION 422 7.2.1 APPLICATION: SITE-TRACK 422 7.3 ANGLES-ONLY
OBSERVATIONS 429 7.3.1 LAPLACE'S METHOD 431 7.3.2 GAUSS'S TECHNIQUE 435
7.3.3 DOUBLE R-ITERATION 439 7.4 MIXED OBSERVATIONS 445 7.4.1 RANGE AND
RANGE-RATE PROCESSING 446 7.4.2 RANGE-ONLY PROCESSING 448 7.5 THREE
POSITION VECTORS AND TIME 450 7.5.1 GIBBS METHOD 450 7.5.2 HERRICK-GIBBS
457 7.6 TWO POSITION VECTORS AND TIME*LAMBERT'S PROBLEM 464 7.6.1
LAMBERT*MINIMUM ENERGY 465 7.6.2 LAMBERT*GAUSS'S SOLUTION 472 7.6.3
LAMBERT'S PROBLEM*THOME'S SOLUTON 476 7.6.4 LAMBERT*UNIVERSAL VARIABLES
485 7.6.5 LAMBERT SOLUTION*BATTIN METHOD 490 7.7 APPLICATION: TARGETING
PROBLEM 495 CHAPTER 8 SPECIAL PERTURBATION TECHNIQUES 515 8.1 HISTORICAL
BACKGROUND 515 8.2 INTRODUCTION TO PERTURBATIONS 516 8.3 ENCKE'S
FORMULATION 521 8.4 COWELL'S FORMULATION 523 8.5 NUMERICAL INTEGRATION
METHODS 524 8.5.1 IMPLEMENTING AN INTEGRATOR AND DETERMINING STEP SIZE
533 8.6 DISTURBING FORCES 536 8.6.1 GRAVITY FIELD OF A CENTRAL BODY 536
8.6.2 ATMOSPHERIC DRAG 549 8.6.3 THIRD-BODY PERTURBATIONS 571 8.6.4
SOLAR-RADIATION PRESSURE 574 8.6.5 OTHER PERTURBATIONS 580 8.7 FORMING
NUMERICAL SOLUTIONS 587 8.7.1 APPLICATION: SIMPLIFIED ACCELERATION MODEL
589 8.7.2 APPLICATION: COMPLEX ACCELERATION MODEL 592 8.8 PRACTICAL
CONSIDERATIONS 595 8.8.1 VERIFYING AND VALIDATING THE PROPAGATOR 596
8.8.2 PHYSICAL DATA AND SOURCES 597 CHAPTER 9 GENERAL PERTURBATION
TECHNIQUES 605 9.1 HISTORICAL BACKGROUND 605 9.2 INTRODUCTION 609 9.2.1
THE METHOD OF PERTURBATIONS '* 613 9.3 VARIATION OF PARAMETERS 615 9.3.1
LAGRANGIAN VOP (CONSERVATIVE EFFECTS) 617 9.3.2 GAUSSIAN VOP
(NONCONSERVATIVE AND CONSERVATIVE EFFECTS) 624 9.4 HAMILTON'S
FORMULATION 633 9.5 DISTURBING-POTENTIAL FORMULATIONS 637 9.5.1 GRAVITY
POTENTIAL IN TERMS OF THE SATELLITE'S ORBITAL ELEMENTS 637 9.5.2
THIRD-BODY POTENTIAL IN TERMS OF THE SATELLITE'S ORBITAL ELEMENTS 639
9.5.3 TIDAL-MOTION POTENTIAL IN TERMS OF THE SATELLITE'S ORBITAL
ELEMENTS 641 9.6 LINEARIZED PERTURBATIONS AND EFFECTS 642 9.6.1
CENTRAL-BODY ANALYSIS 643 9.6.2 DRAG ANALYSIS 667 9.6.3 THIRD-BODY
ANALYSIS 675 9.6.4 SOLAR-RADIATION ANALYSIS 681 9.7 FORMING ANALYTICAL
SOLUTIONS 685 9.7.1 APPLICATION: PERTURBED TWO-BODY PROPAGATION 686 |
| adam_txt |
FUNDAMENTALS OF ASTRODYNAMICS AND APPLICATIONS THIRD EDITION DAVID A.
VALLADO WITH TECHNICAL CONTRIBUTIONS BY WAYNE D. MCCLAIN SPACE
TECHNOLOGY LIBRARY PUBLISHED JOINTLY BY MICROCOSM PRESS HAWTHORNE, CA
SPRINGER NEW YORK, NY TABLE OF CONTENTS VLL CHAPTER 1 EQUATIONS OF
MOTION 1.1 CHAPTER 2 CHAPTER 3 1.2 1.3 HISTORY .1.1 ANCIENT ERA . 1.2
THE COPERNICAN REVOLUTION .1.3 KEPLER'S LAWS .1.4 NEWTON'S LAWS .1.5
OTHER EARLY ASTRODYNAMIC CONTRIBUTIONS GEOMETRY OF CONIC SECTIONS .2.1
BASIC PARAMETERS TWO-BODY EQUATION .3.1 ASSUMPTIONS FOR THE TWO-BODY
EQUATION .3.2 SPECIFIC ANGULAR MOMENTUM .3.3 SPECIFIC MECHANICAL ENERGY
.3.4 KEPLER'S FIRST LAW (TRAJECTORY EQUATION) .3.5 KEPLER'S SECOND AND
THIRD LAWS .3.6 VELOCITY FORMULAS 1.4 THREE-BODY AND -BODY EQUATIONS
1.4.1 INERTIAL, RELATIVE, AND BARYCENTRIC FORMULAS 1.4.2 TEN KNOWN
INTEGRALS 1.4.3 GENERAL THREE-BODY PROBLEM KEPLER'S EQUATION AND
KEPLER'S PROBLEM 2.1 HISTORICAL BACKGROUND 2.2 KEPLER'S EQUATION 2.2.1
ALTERNATE FORMULATION FOR ECCENTRIC ANOMALY 2.2.2 FORMULATION FOR THE
PARABOLIC ANOMALY 2.2.3 FORMULATION FOR THE HYPERBOLIC ANOMALY 2.2.4
UNIVERSAL FORMULATION 2.2.5 SOLUTIONS OF KEPLER'S EQUATION 2.2.6 SUMMARY
AND RELATED FORMULAS 2.3 KEPLER'S PROBLEM 2.3.1 SOLUTION TECHNIQUES 2.4
SATELLITE STATE REPRESENTATIONS 2.4.1 CLASSICAL ORBITAL ELEMENTS
(KEPLERIAN) 2.4.2 TWO-LINE ELEMENT SETS 2.4.3 OTHER ELEMENT SETS 2.4.4
CANONICAL ELEMENTS 2.5 APPLICATION: ORBITAL ELEMENTS FROM R AND V 2.6
APPLICATION: R AND V FROM ORBITAL ELEMENTS 2.7 APPLICATION: GROUNDTRACKS
2.8 APPLICATION: FIND TIME OF FLIGHT (FINDTOF) COORDINATE AND TIME
SYSTEMS 3.1 HISTORICAL BACKGROUND 3.2 THE EARTH 3.2.1 LOCATION
PARAMETERS 3.2.2 SHAPE OF THE EARTH 3.2.3 GRAVITATIONAL MODEL 1 1 7 9 10
12 12 12 20 23 23 25 27 29 32 33 33 37 40 49 49 51 57 58 60 66 71 85 87
88 103 104 113 116 118 119 124 128 131 137 137 139 141 142 149 VLLL 3.3
COORDINATE SYSTEMS 153 3.3.1 INTERPLANETARY SYSTEMS 158 3.3.2
EARTH-BASED SYSTEMS 159 3.3.3 SATELLITE-BASED SYSTEMS 162 3.4 COORDINATE
TRANSFORMATIONS 166 3.4.1 COORDINATE ROTATION 167 3.4.2 ROTATING
TRANSFORMATIONS 173 3.4.3 COMMON TRANSFORMATIONS 174 3.4.4 APPLICATION:
CONVERTING UK (ECEF) TO LATITUDE AND LONGITUDE 176 3.5 TIME 181 3.5.1
SOLAR TIME AND UNIVERSAL TIME 184 3.5.2 SIDEREAL TIME 191 3.5.3 ATOMIC
TIME 196 3.5.4 DYNAMICAL TIME 197 3.5.5 COORDINATE TIME 200 3.5.6
CONVERSIONS 201 3.6 TIME CONVERSIONS 203 3.6.1 DMS TO RAD / RAD TO DMS
203 3.6.2 HMS TO RAD / RAD TO HMS 204 3.6.3
HMSTOTIMEOFDAY/TIMEOFDAYTOHMS 205 3.6.4 YMD TO DAY OF YEAR/DAY OF YEAR
TO YMD 206 3.6.5 YMDHMSTODAYS/DAYSTOYMDHMS 207 3.6.6 JULIAN DATE TO
GREGORIAN DATE 208 3.7 TRANSFORMING CELESTIAL AND TERRESTRIAL
COORDINATES 209 3.7.1 IAU-2000 RESOLUTIONS 217 3.7.2 VELOCITY
TRANSFORMATIONS 227 3.7.3 IAU-76 / FK5 REDUCTION 228 3.7.4 OTHER
REDUCTIONS 236 3.7.5 COMPUTATIONAL CONSIDERATIONS 240 3.8 EARTH MODELS
AND CONSTANTS 242 3.8.1 CANONICAL UNITS 242 CHAPTER 4 OBSERVATIONS 247
4.1 INTRODUCTION 247 4.2 OBTAINING DATA 248 4.2.1 QUANTITY OF DATA : 251
4.2.2 TYPES OF DATA 252 4.2.3 EXAMPLE APPLICATIONS 253 4.3 INTRODUCTION
TO SENSOR SYSTEMS 254 4.4 OBSERVATION TRANSFORMATIONS 258 4.4.1
GEOCENTRIC RIGHT ASCENSION AND DECLINATION 260 4.4.2 TOPOCENTRIC RIGHT
ASCENSION AND DECLINATION 263 4.4.3 AZIMUTH-ELEVATION 265 4.4.4
PRACTICAL AZ-EL CONVERSIONS 270 4.4.5 TRANSFORMATIONS FOR ECLIPTIC
LATITUDE AND LONGITUDE 272 4.4.6 PRACTICAL ASPECTS OF SURVEILLANCE 274
CHAPTER 5 CELESTIAL PHENOMENA 279 5.1 SOLAR PHENOMENA 279 5.1.1
APPLICATION: SUN POSITION VECTOR 279 5.1.2 APPLICATION: SUNRISE, SUNSET,
AND TWILIGHT TIMES 283 IX 5.2 LUNAR PHENOMENA 287 5.2.1 APPLICATION:
MOON POSITION VECTOR 288 5.2.2 APPLICATION: MOON RISE AND SET TIMES 292
5.2.3 PHASES OF THE MOON 296 5.3 CELESTIAL APPLICATIONS 296 5.3.1
APPLICATION: PLANETARY EPHEMERIDES 297 5.3.2 ECLIPSES 300 5.3.3
APPLICATION: SIGHT AND LIGHT 307 5.3.4 GROUND ILLUMINATION 311 5.3.5
MISCELLANEOUS PHENOMENA 313 CHAPTER 6 ORBITAL MANEUVERING 319 6.1
HISTORICAL BACKGROUND 319 6.2 INTRODUCTION 320 6.3 COPLANAR MANEUVERS
322 6.3.1 HOHMANN AND BI-ELLIPTIC TRANSFERS 324 6.3.2 COMPARING HOHMANN
AND BI-ELLIPTIC TRANSFERS 330 6.3.3 TRANSFERS USING THE ONE-TANGENT BURN
333 6.3.4 GENERAL TRANSFERS 339 6.4 NONCOPLANAR TRANSFERS 339 6.4.1
INTRODUCTION 339 6.4.2 INCLINATION-ONLY CHANGES 344 6.4.3 CHANGES IN THE
RIGHT ASCENSION OF THE ASCENDING NODE 347 6.4.4 CHANGES TO INCLINATION
AND THE ASCENDING NODE 350 6.5 COMBINED MANEUVERS 352 6.5.1
MINIMUM-INCLINATION MANEUVERS 353 6.5.2 FIXED-AL? MANEUVERING 356 6.6
CIRCULAR RENDEZVOUS 360 6.6.1 CIRCULAR COPLANAR PHASING 360 6.6.2
CIRCULAR NONCOPLANAR PHASING 367 6.7 CONTINUOUS-THRUST TRANSFERS . 373
6.7.1 INTRODUCTION 374 6.7.2 ORBIT RAISING 377 6.7.3 LOW-THRUST,
NONCOPLANAR TRANSFERS 383 6.8 RELATIVE MOTION 389 6.8.1 POSITION
SOLUTIONS FOR NEARLY CIRCULAR ORBITS 394 6.8.2 TREND ANALYSIS 398 6.8.3
ACCURACY ANALYSIS 412 CHAPTER 7 INITIAL ORBIT DETERMINATION 419 7.1
HISTORICAL BACKGROUND 419 7.2 OBSERVATIONS OF RANGE, AZIMUTH, AND
ELEVATION 422 7.2.1 APPLICATION: SITE-TRACK 422 7.3 ANGLES-ONLY
OBSERVATIONS 429 7.3.1 LAPLACE'S METHOD 431 7.3.2 GAUSS'S TECHNIQUE 435
7.3.3 DOUBLE R-ITERATION 439 7.4 MIXED OBSERVATIONS 445 7.4.1 RANGE AND
RANGE-RATE PROCESSING 446 7.4.2 RANGE-ONLY PROCESSING 448 7.5 THREE
POSITION VECTORS AND TIME 450 7.5.1 GIBBS METHOD 450 7.5.2 HERRICK-GIBBS
457 7.6 TWO POSITION VECTORS AND TIME*LAMBERT'S PROBLEM 464 7.6.1
LAMBERT*MINIMUM ENERGY 465 7.6.2 LAMBERT*GAUSS'S SOLUTION 472 7.6.3
LAMBERT'S PROBLEM*THOME'S SOLUTON 476 7.6.4 LAMBERT*UNIVERSAL VARIABLES
485 7.6.5 LAMBERT SOLUTION*BATTIN METHOD 490 7.7 APPLICATION: TARGETING
PROBLEM 495 CHAPTER 8 SPECIAL PERTURBATION TECHNIQUES 515 8.1 HISTORICAL
BACKGROUND 515 8.2 INTRODUCTION TO PERTURBATIONS 516 8.3 ENCKE'S
FORMULATION 521 8.4 COWELL'S FORMULATION 523 8.5 NUMERICAL INTEGRATION
METHODS 524 8.5.1 IMPLEMENTING AN INTEGRATOR AND DETERMINING STEP SIZE
533 8.6 DISTURBING FORCES 536 8.6.1 GRAVITY FIELD OF A CENTRAL BODY 536
8.6.2 ATMOSPHERIC DRAG 549 8.6.3 THIRD-BODY PERTURBATIONS 571 8.6.4
SOLAR-RADIATION PRESSURE 574 8.6.5 OTHER PERTURBATIONS 580 8.7 FORMING
NUMERICAL SOLUTIONS 587 8.7.1 APPLICATION: SIMPLIFIED ACCELERATION MODEL
589 8.7.2 APPLICATION: COMPLEX ACCELERATION MODEL 592 8.8 PRACTICAL
CONSIDERATIONS 595 8.8.1 VERIFYING AND VALIDATING THE PROPAGATOR 596
8.8.2 PHYSICAL DATA AND SOURCES 597 CHAPTER 9 GENERAL PERTURBATION
TECHNIQUES 605 9.1 HISTORICAL BACKGROUND 605 9.2 INTRODUCTION 609 9.2.1
THE METHOD OF PERTURBATIONS '* 613 9.3 VARIATION OF PARAMETERS 615 9.3.1
LAGRANGIAN VOP (CONSERVATIVE EFFECTS) 617 9.3.2 GAUSSIAN VOP
(NONCONSERVATIVE AND CONSERVATIVE EFFECTS) 624 9.4 HAMILTON'S
FORMULATION 633 9.5 DISTURBING-POTENTIAL FORMULATIONS 637 9.5.1 GRAVITY
POTENTIAL IN TERMS OF THE SATELLITE'S ORBITAL ELEMENTS 637 9.5.2
THIRD-BODY POTENTIAL IN TERMS OF THE SATELLITE'S ORBITAL ELEMENTS 639
9.5.3 TIDAL-MOTION POTENTIAL IN TERMS OF THE SATELLITE'S ORBITAL
ELEMENTS 641 9.6 LINEARIZED PERTURBATIONS AND EFFECTS 642 9.6.1
CENTRAL-BODY ANALYSIS 643 9.6.2 DRAG ANALYSIS 667 9.6.3 THIRD-BODY
ANALYSIS 675 9.6.4 SOLAR-RADIATION ANALYSIS 681 9.7 FORMING ANALYTICAL
SOLUTIONS 685 9.7.1 APPLICATION: PERTURBED TWO-BODY PROPAGATION 686 |
| any_adam_object | 1 |
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| author | Vallado, David A. |
| author_facet | Vallado, David A. |
| author_role | aut |
| author_sort | Vallado, David A. |
| author_variant | d a v da dav |
| building | Verbundindex |
| bvnumber | BV022869222 |
| classification_rvk | US 1200 |
| classification_tum | VER 843f |
| ctrlnum | (OCoLC)253958501 (DE-599)DNB983501351 |
| dewey-full | 629.41 |
| dewey-hundreds | 600 - Technology (Applied sciences) |
| dewey-ones | 629 - Other branches of engineering |
| dewey-raw | 629.41 |
| dewey-search | 629.41 |
| dewey-sort | 3629.41 |
| dewey-tens | 620 - Engineering and allied operations |
| discipline | Physik Verkehrstechnik Verkehr / Transport |
| discipline_str_mv | Physik Verkehrstechnik Verkehr / Transport |
| edition | 3. ed. |
| format | Book |
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| id | DE-604.BV022869222 |
| illustrated | Illustrated |
| index_date | 2024-07-02T18:46:33Z |
| indexdate | 2025-01-27T13:01:14Z |
| institution | BVB |
| isbn | 9780387718316 9781881883142 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-016074354 |
| oclc_num | 253958501 |
| open_access_boolean | |
| owner | DE-706 DE-91G DE-BY-TUM DE-83 DE-20 |
| owner_facet | DE-706 DE-91G DE-BY-TUM DE-83 DE-20 |
| physical | XXI, 1055 S. graph. Darst. |
| publishDate | 2007 |
| publishDateSearch | 2007 |
| publishDateSort | 2007 |
| publisher | Microcosm Press [u.a.] |
| record_format | marc |
| series | Space technology library |
| series2 | Space technology library |
| spelling | Vallado, David A. Verfasser aut Fundamentals of astrodynamics and applications David A. Vallado 3. ed. Hawthorne, Calif. Microcosm Press [u.a.] 2007 XXI, 1055 S. graph. Darst. txt rdacontent n rdamedia nc rdacarrier Space technology library 21 Astrodynamik (DE-588)4143246-0 gnd rswk-swf Satellitendynamik (DE-588)4206759-5 gnd rswk-swf Satellitendynamik (DE-588)4206759-5 s DE-604 Astrodynamik (DE-588)4143246-0 s 1\p DE-604 Space technology library 21 (DE-604)BV010116374 21 GBV Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=016074354&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis 1\p cgwrk 20201028 DE-101 https://d-nb.info/provenance/plan#cgwrk |
| spellingShingle | Vallado, David A. Fundamentals of astrodynamics and applications Space technology library Astrodynamik (DE-588)4143246-0 gnd Satellitendynamik (DE-588)4206759-5 gnd |
| subject_GND | (DE-588)4143246-0 (DE-588)4206759-5 |
| title | Fundamentals of astrodynamics and applications |
| title_auth | Fundamentals of astrodynamics and applications |
| title_exact_search | Fundamentals of astrodynamics and applications |
| title_exact_search_txtP | Fundamentals of astrodynamics and applications |
| title_full | Fundamentals of astrodynamics and applications David A. Vallado |
| title_fullStr | Fundamentals of astrodynamics and applications David A. Vallado |
| title_full_unstemmed | Fundamentals of astrodynamics and applications David A. Vallado |
| title_short | Fundamentals of astrodynamics and applications |
| title_sort | fundamentals of astrodynamics and applications |
| topic | Astrodynamik (DE-588)4143246-0 gnd Satellitendynamik (DE-588)4206759-5 gnd |
| topic_facet | Astrodynamik Satellitendynamik |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=016074354&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
| volume_link | (DE-604)BV010116374 |
| work_keys_str_mv | AT valladodavida fundamentalsofastrodynamicsandapplications |