Applied orbit perturbation and maintenance:
Gespeichert in:
| Hauptverfasser: | , |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
El Segundo, California
The Aerospace Press
[2018]
Reston, Virginia American Institute of Aeronautics and Astronautics, Inc. |
| Ausgabe: | second edition |
| Schlagworte: | |
| Online-Zugang: | Inhaltsverzeichnis |
| Beschreibung: | Includes bibliographical references and index |
| Beschreibung: | xviii, 411 Seiten |
| ISBN: | 1884989276 9781884989278 |
Internformat
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| 100 | 1 | |a Chao, Chia-Chun |d 1939- |e Verfasser |0 (DE-588)1215275773 |4 aut | |
| 245 | 1 | 0 | |a Applied orbit perturbation and maintenance |c Chia-Chun "George" Chao and Felix R. Hoots |
| 250 | |a second edition | ||
| 264 | 1 | |a El Segundo, California |b The Aerospace Press |c [2018] | |
| 264 | 1 | |a Reston, Virginia |b American Institute of Aeronautics and Astronautics, Inc. | |
| 264 | 4 | |c © 2018 | |
| 300 | |a xviii, 411 Seiten | ||
| 336 | |b txt |2 rdacontent | ||
| 337 | |b n |2 rdamedia | ||
| 338 | |b nc |2 rdacarrier | ||
| 500 | |a Includes bibliographical references and index | ||
| 650 | 4 | |a Artificial satellites |x Orbits | |
| 650 | 4 | |a Orbital mechanics | |
| 650 | 4 | |a Perturbation (Mathematics) | |
| 650 | 0 | 7 | |a Umlaufbahn |0 (DE-588)4238276-2 |2 gnd |9 rswk-swf |
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| 689 | 0 | 2 | |a Störung |0 (DE-588)4133232-5 |D s |
| 689 | 0 | |5 DE-604 | |
| 700 | 1 | |a Hoots, Felix R. |d 1947- |e Verfasser |0 (DE-588)1215279604 |4 aut | |
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| 943 | 1 | |a oai:aleph.bib-bvb.de:BVB01-030463775 | |
Datensatz im Suchindex
| _version_ | 1806053919821922304 |
|---|---|
| adam_text |
Contents
Preface XV
Acknowledgments xvii
Source Notes w resecsssesssscsssssssccssvessssssssesssecsssssensvscssuessassctsssssseysusaseanavesausessscceuseece xvii
Chapter 1 A Review of Two-Body Mechanics
1 1 Kepler’s Laws
Chapter 2 Equations of Motion with Perturbations c 00000 9
2 1, General Equations of Motion in Earth-Centered Inertial Coordinates for
Gravity Harmonics cccsssssssessesseecsscssssessssssessvecseseussavansrsscessszaseacesssseceeseens 10
2 2 Third-Body (Sun-Moon) Attractions csssscssssssssssssseceesestscseseseenserssesatareaes 12
2 3 Solar-Radiation Pressure
2 4, Atmospheric Drag cssssessessssstscsecseccsecessucssveseesnesnsesesssesensucesoueaseuseeeaseensess
2 5 Other Small Forces for High-Precision Orbit Prediction
251 Solid Tides oo
252 Ocean Tides
253 Relativistic Effects cecssscsssssesesssseececceeessscssssensescensasessscarserseeneees
254 Earth Radiation eseeesteenennenenteneerensnsnsensnsensenensnennestnesssnssaensensnsnsnsnann
255 Yarkovsky Forces keensenenssensensessuunananane
256 Planetary Forces uetseaveccovennenenens
2 6 Coordinates and Integration sssssssesssecssessecessecsessseseennssnsenesseeseeaseaeanseasases 17
261 Methods of Integration ae 18
262 Numerical Integration Methods and TOOIdS sssssssecssssonscsnsssessessersersees 18
2 7, References sccccsscsscccessroeerescccsessesessscacatsnscsvseseauevsastorseseacecssscatneasarscaratarsenees 19
Chapter 3 Averaged Equations of Motion in Classical
Elements 21
3 1 Background of General Perturbations ssssssssssrsessssssessssnsssssensseccnesseses 21
3 2 Method of Averaging c csscecssecsescnsssussssessessssssssssessasseasensesssessssssrecsesseseers 22
3 3 Averaged Equations for Earth Zonal Harmonics sssssssessescssessecsneesesenes 28
3 4 Averaged Equations for Sun-Moon Gravitational Perturbations 00 0 33
3 5 Averaged Equations for Solar-Radiation Pressure sesssssssccsessessesssseesees 41
3 6 Averaged Equations for Earth Atmospheric Drag 47
3 7 Removal of Singularities unensesenesssensensensensenesnnenssuennnnnnnunnnennennnennennennne 51
3 8 References
Chapter 4 Resonant Tesseral Harmonics in Kaula’s
Formulations 59
41G Function for Eccentricity Series sesateccauaeeseseauesceneesererarstsetsetereestotens 60
42F Function for Inclination Series unse 63
4 3 Generalized Equations of Variation in Terms of F and G Functions 67
4 4 Equilibrium Longitudes for 24~Hour Orbits c scccssssssesssecssssessesesseseesecesses 68
441 Sensitivity to Eccentricity and Argument of Perigee u 74
4 5 Equilibrium Longitudes for 12-Hour Circular Orbits can 74
4 6 Equilibrium Longitudes for 12-Hour Molniya Orbits ssssccsssssssesessssssssees 75
4 7 References
Chapter 5 The SGP4 Orbit Prediction Model and Its
Application
5 1, History and Assumptions scccccscsssseessescssene
5 2 Simplified Equations of Motion
5 3 Use Of SGP4 sssssssssssssssccsnscsssssssessessussssssvsccessveserssessersasacasasessarsenecesesuscescese
5 5 Improved Ephemeris Predictions with SGP4/TLE
551 Three Sample Cases of GEO Ephemeris Prediction Improvement 86
552 Reentry Date and Time Predictions of Phobos-Grunt Spacecraft 88
553 Automated Ballistic Coefficient Estimation Technique and
Application sssscssssscstsesssvessssssassvusssassecsserssassessasssestesssecsssessessssessess 90
5 6 References
Chapter 6 Application of Averaged Equations to Orbit
Analysis 97
6 1 Long-Term Eccentricity and Inclination Variations in Geosynchronous Orbits 97
611 Eccentricity Variation Induced by Solar-Radiation Pressure 97
612 Inclination Variation Induced by Sun/Moon Attractions 99
6 2 Long-Term Eccentricity and Inclination Variations in Medium Earth
Orbits (GPS Orbits) ccsccseeseccsssesssssessscsessusssessesseccacencesecsarersesuecateneenecens 103
621 GPS Disposal Orbit Stability cccssssscssssccssssssssesesssescssessesersacerese 103
622 GPS Inclination Variation csssecssssssscescsssssecsesssesscsececsecuecaseenseeves 105
6 3 Long-Term Eccentricity and Inclination Variations in Highly Elliptical
Orbits (Molniya and GTO) ccsscsecescsccesecssccsesecsessssesccenscseecene 106
631 Inclination Variation ccscssssssssssssssessssseessessecssseceesaseccecseerecsaseness 107
632 Eccentricity Variation cccccsscssssssssssssesssesessessvsecereceersacsrsarecssnseces 107
6 4 Resonance Effects in Gravity, Solar-Radiation Pressure, and Third-Body
Equations for Low Barth Orbits c ccsssessssessssesssssrsesssseeeesscersessesessesses 109
6 4 1, Resonance Effects Resulting from Third-Body Attractions 109
6 4 2, Resonance Effects Resulting from Earth Gravity and Solar-
Radiation Pressure sssssesssscscsssseceessassesssssscssecsesessssssesneseseaueees 111
6 5 J3 Effects and Frozen Orbits cccccsssssecesssssssseseerssstesasatessssassssescenseeseess 112
6 6 References
Chapter 7 Orbit Maintenance of LEO, MEO, and HEO
Satellites and Constellations cccsscssssessessssersesseeee LL 9
7 1, Orbit Maintenance of LEO Satellites and Constellations :sessese 120
711 Orbit Maintenance of LEO Satellites eeeneenenennennnene 120
712 Maintenance of LEO Constellations ueuesseneseneesensneensnnennesnennenen 123
7 2 Maintenance of GPS and Other MEO Constellations ueesenereeseeesesneeenn 126
721 GPS Constellation History and Reference Frame „nenne 126
7 2 2, Inclination Biasing and Longitude Stationkeeping Method for GPS 128
723 Effects of GPS Stationkeeping on Mission Performance 06 131
7 24 Other MEO Constellation Control Strategies ccscssssssecsessseaes 132
7 3 Maintenance of Molniya Orbits and Other HEO Constellations 132
7 3 1, Longitude Stationkeeping of Molniya Orbits sssssussesessenees 132
732 Long-Term Eccentricity Variation of Molniya Orbits „nen 133
733 Perturbations and Control of Three-Hour Magic Orbits 134
74 Guidelines for Designing Orbit Analysis Tools cccssessssersesseesseseerses 136
7 5 References ensesennseresneereensnnnensnenensoenenensararsesnenssnensensnesrsensnsensnsnenenerssssesnen 140
8 1 Longitude (East-West) Stationkeeping
811 Simplified Equations for Spacecraft Motion Between
Stationkeeping Maneuvers uesneensnennsonnsnnsentontnenensenenensnnastensnasensnn 145
812 True Longitude Variations and Stationkeeping Limit 148
8 2 Inclination (North-South) Stationkeeping u cnensenenesnseesensennnensnennonennenneennee 149
8 3 Solar-Radiation Pressure and the Sun-Pointing Strategy 151
831 Option with No Additional Fuel unessernsseensensnnnensonnennensreonesenenne
832 Options with Additional Fuel
833 Argument of Perigee Control Strategies cccssssssssssssesseeseesseeees
8 4 Perturbations and Control of Tundra Orbits cccssssessserssecssesecsesssseceees
841 Optimal RAAN Strategy cccscsessscssseseessecersees
842A Strategy with Frozen or Nearly Frozen Orbits
843 Optimized Inclination Strategy cccsssssosseseeseesseecsssceteascecesesesvees
8 5 Guidelines for Designing GEO Orbit Analysis Tools cscsscrsnseee
851 Recommended Force Models and Precision
852 Summary of Capabilities 0 0 cssssssessessssersessessessesessscesessensessecenas
853 Sample Input Description cccessssccssessssesssseeseceessssesscsecesareeseavense
8531 Long-Term Propagation Without Stationkeeping
Simulation unesesnsessessneensonsorenssnneenesnusnnsannonenenennennennenennn 164
8532 Propagation with Stationkeeping Simulation 165
8533 Station Visibility «u ccmsseseensseesssensnnensenennensnnennennenennnnnneenn 166
853 4, Eclipse Window cccsssessssssssssecsssesssssccsseccacseesessesseateueeecaes 166
854 Postprocessing c cccessscsssessessesssossessssussossssvesesassesatarecucssecansasserseves 166
8 6 Stationkeeping Using Ion Propulsion se ccsscsscsscsssssesscessccsressecssecsesereeese 166
8 7 References sssssssscosscseesscssvesssessesssccsscsssssuseasscsssanensessecsessserseseuecsaeesanenavens 171
Chapter 9 Collocation of GEO Satellites csccssscssssssscsssseveesd 73
9 1 ITU Policies and the Need for Collocation men 173
911 Policies and Functions of ITU
912 Need for Collocation ceccssscsscseessvesssesssssssasssssscesessecsavessusesuteeneeses
9 2 Strategies of GEO Collocation csssscsecsscsscessessucsnssesecsessescesserearcosseseesse
921 The Complete Longitude Separation Strategy ccsssecscssessccnsesccreees 175
922 Coordinated Stationkeeping Strategy cscccssssescsescsesesesesseseeseeses 175
Contents ix
922 1, Equations for Radial Separation unsesnsneenesenneessenueneene 176
9222 Equations for Cross-Track Separation ssssssssssssesereessee 178
9223A Strategy for Coordinated Stationkeeping Maneuvers 179
922 4, Numerical Example of Two-Satellite Collocation 181
9225 Numerical Example of Three-Satellite Collocation 183
923 The Eccentricity-and-Inclination Separation Strategy 185
9231 Eccentricity Vector Separation sssssssssssssscccseseccaneccernenecs 186
9232 Eccentricity and Inclination (e-i) Vector Separation 191
9 2 4, The Halo Separation Strategy cssccesccssscsssscssescssesestesessesasserectecerece 194
924 1, Mathematical Derivation of a Halo Suborbit we 195
924 2, Relations for Determining a Halo Suborbit cc sescsssesse 196
9243 Control of the Halo Formation with the BEP Method 197
9244 Control of Halo Formation via Autofeedback Controller
with Onboard GPS uesneessssnsenssensennenneonnneusnnnnennennennenn 199
9 3 Operational Requirements for Collocation Maintenance aan 201
9 4 Collision Avoidance Strategies ccscssssssessssscssscrsesssssnsscsereresecsessssessesssseses 202
9 4 1, Risk Assessment and Algorithms for Computing Probability of
COILSION csceccssscesssessvssscssersoesecsecssecnecavesvecsuessssessuserssasceneesecseveavens 203
942 Operational Processing and Collision Avoidance Strategies 203
9,5, REFELENCES scsssssssessessssseecscsseessecsecsessessccssssnssuusasesnscasessecsacenetsescesersersenseces 204
Chapter 10 Advanced Concepts of Orbit Control 000000 207
10 1 Autonomous Onboard Stationkeeping of GEO Satellites Using GPS 207
10 2 Autonomous Formationkeeping of Cluster Satellites via Relative
Ranging essen Anerssnsnssssnsnssntsssssssssnenssssnentesssessentsosstunsanae 215
10 2 1 Formationkeeping of LEO Cluster Satellites for a Sparse Array
AMICMNA scssscssssscseseseersnesesesescesersatersessaseadatsseeesesesenecaseeseesesensnnsess
10 211 Populating a Cluster Orbit
10, 212 Perturbation Effects and Formationkeeping Strategy 221
10 213 Stationkeeping Strategy for the Center Satellite 226
10 2 2 Formationkeeping of a Halo Suborbit for Space Solar Power
Collectors cssesesesssseracunsnenennnenenenennnnn vrsesesarueneneens 227
10 2 3 Generation of Roll and Yaw History Plots senesneeeneneneneueonuunn 231
10 3 Deployment of Wheel Cluster Satellite Formations with Control
Algorithms 000000s0nesosnsnrnrsensneensnentnentsnstnnsesnsssnsnnnenenensonsosonessrnsnanenn 233
10 3 1 Extended Wheel Cluster Formation Concept uesseresenssnonenserunnnn 233
10 3 2 Application to Highly Elliptical Orbits ueeseseeseesessnsnssonunnennnns 237
10 3 3 Strategies for Wheel Cluster Formationkeeping scceesen 237
10 3 4 Control Algorithms for Near-Circular Orbits cccssssseseesseseees 241
x Contents
10 3 5 Control Algorithm for Elliptical Orbits ereneeesesensennensersenenenennnnenn 243
10 4 References sccccsssssessesssceseesessesnccusentensusavausseensacerseueasnsaeesseaceeasatenteceaeees 243
Chapter 11 End-of-Life Disposal Orbits: Strategies and Long-
Term Stability 247
11 1 Policies for End-of-Life Disposal of Satellites
11 2 Study 1: Stability of GEO Disposal Orbits ccsssesessesesesssecsssstscesssvens
11 2 1 Study 1 (GEO Disposal Orbit Stability): Introduction 250
11 2 2 Study 1 (GEO Disposal Orbit Stability): Approach 251
11 2 3 Study 1 (GEO Disposal Orbit Stability): Analytical
Investigation eenessssssnsnsusennnnnensnenennsnnensnsarnensonnenssnnnanannurnnenennen 251
11 231 Eccentricity Variation Based on Singly Averaged
Equations euesssssesennsesenensnnnnnnnonenennonensnensnesssesenensenennaner 252
11 232 Eccentricity Variation Based on Doubly Averaged
Equations ceeseesensesesesensnnenensnnnneonnonnensnssssnsessssssnennsssennnenn 253
11 2 4 Study 1 (GEO Disposal Orbit Stability): Numerical Integration 253
11 241 Force Models and Initial Conditions of 100-Year
Integrations cessesenensesenensnsnnensonnsenenessennnnsnnsersnannnnnnennn 253
11 242 Results of 100- Year Integration s cssscssssessssssessesees 254
11 243 TRACE Results cnensesesesssenesnenennnnsnennosennnannnnnennnnnennne 258
11 2 5 Study 1 (GEO Disposal Orbit Stability): Conclusions 261
11 2 6 Study I (GEO Disposal Orbit Stability): Recommendations 261
11 3 Study 2: MEO Disposal Orbit Stability and Direct Reentry Strategy 263
11 3 1 Study 2 (MEO Disposal Orbit Stability): Introduction au 263
11 3 2, Study 2 (MEO Disposal Orbit Stability): Approach can 264
11 3 3 Study 2 (MEO Disposal Orbit Stability): Analytical
Investigation 0 sccssessssssssssssesssssssecerssersssecasarsretscsusessesarsassersoes 265
11 331 Eccentricity Variation Based on Singly Averaged
Equations (for MEO Orbits Between 2000 and 4000 km
Altitude) cecsssscssessesseessesssnsessessssucenscuseuesecsesssenerseensenees 265
11 332 Discovery of Large Eccentricity Growth of GPS Disposal
Orbits (Based on Doubly Averaged Equations) 00 266
11 333 Eccentricity Variation Based on Doubly Integrated
Equations (for Molniya and GTO Orbits) uenn 268
11 3 4 Study 2 (MEO Disposal Orbit Stability): Numerical Integration 269
11 341 Force Models and Initial Conditions of Long-Term
Entegration c scscssessscsesssesssesssessesssssseesensoecatsscessacssetese
11 342 Results of MEANPROP Integration
11 343 TRACE and MEANPROP Comparison
11 3 5, Study 2 (MEO Disposal Orbit Stability): Direct Reentry Strategy 278
11 3 6 Study 2 (MEO Disposal Orbit Stability): Conclusions 0 0 281
11 4
Chapter 12 Space Debris
Contents = xi
11 3 7, Study 2 (MEO Disposal Orbit Stability): Recommendations 282
Study 3: Long-Term Evolution of Navigation Satellite Orbits: GPS/
GLONASS/Galileo cceceae 283
11 4 1 Study 3 (Navigation Satellite Orbits): Introduction nee 283
11 4 2 Study 3 (Navigation Satellite Orbits): Analytical Investigation 284
11 4 3 Study 3 (Navigation Satellite Orbits): Long-Term Numerical
Propagation Studies ccsssesssssssesssesssssssceccessssceresssessassssessvecseees 285
11 4 4 Study 3 (Navigation Satellite Orbits): Dependence on Inclination 286
11 4 5 Study 3 (Navigation Satellite Orbits): Conclusions „aa 288
Study 4: Reentry Disposal for LEO Spacecraft ccscscssssssesssescssessesecsee 289
11 5 1 Study 4 (Reentry Disposal for LEO Spacecraft): Introduction 289
11 5 2 Study 4 (Reentry Disposal for LEO Spacecraft): Approach 289
11 5 3 Study 4 (Reentry Disposal for LEO Spacecraft): Theory and
ASSUMPTIONS ssscssessccesseesessesssseesnssecsscsnssesstaneesecans 290
11 5 4 Study 4 (Reentry Disposal for LEO Spacecraft): Analysis of
Additional Deorbit Weight usenssesseessneneneonnnenneununennnnnnnnnnnnnn 292
11 5 5 Study 4 (Reentry Disposal for LEO Spacecraft): Analysis of
Collision Probabilities os escessssssssssssssesessessssescecssessvecseencersecnss 296
11 5 6 Study 4 (Reentry Disposal for LEO Spacecraft): Discussion of
Advantages and Disadvantages of Options cccsesseseeseeseeees 298
11 5 7 Study 4 (Reentry Disposal for LEO Spacecraft): Conclusions 301
References ceccsssssssssscsseesssseecsecnecsessecessnnssssessesnesasaussauesesssssecsuceseeseeease 301
The Future Space Debris Environment 0 csssssscsssecsssessesesseessseassoees
Fragmentation Modeling ssssssecsessscesessssseacsseseseceeensenssseessssesseeessneaseses
12 2 1 The Need to Analyze Breakup Events
12 2 2 Sources of Data ueeenenssesnnensenenennennrnnonennenr “
12 2 3 Characteristics of Breakups csssscscssssccesstssessececeeeseeseseenssesseeees
12 2 4 The IMPACT Model sccsssesssscsssscsseseesesecsseceeeessecesessereteceneacenss
12 2 5 Further Developments esenensensnnenensnnnnnenesernrennennnnnne
Situational Awareness Provided by the DART Team cscsssssssesescseees 312
12 3 1 DART Products ereorsensnenonsnsnsenenennusnsensnentessnnnnn
12 3 2 Continued Improvement Efforts
Space Surveillance for Operational Support nsesssssesessssnsnsunensunsennsenensnenen 314
12 4 1 The Space Catalog u neensseesssensessnsnssensseoronuuroennnnsnennsnensnnsnnnsennnn 314
12 4 2 Risk Prediction seseneseveeaeaeeesens 314
12 4 3 Network Upgrades 315
xii Contents
12 5 The Power of the TOruS ccsssscscssesssoreresesccceneeererenesensseeneneateneantentireaseas
12 5 1 The Torus Evolved: Alpha-Shapes uuerereeneneensnssresesnensennsnnntersuneen
12 52A Quicker Response cauesenresennesenssnnnsneserenennorsrensnsnensrssnsnsentnenasnee
12 6 Collision Avoidance for Launch Protection essnessrsersnennenersensentensentorenn
12 7 Disposal and Active Debris Removal cssssssseessereeeereneeness
12 7 1 Postmission Disposal nen
12 7 2 Active Debris Removal nenne
12 7 3 Legal Issues around Active Debris Removal
12 8 Summary aenenseneensenernensnantnannssnessnsstsenenssnnennsssnensuensrossnnussossnsorennn
12 9 References sccssscsssssssecsssssecesesneneesaneenersseseessenerscauenteasaaueeseuoaterntssesvereaes
Chapter 13 Recent Advancements in Atmospheric Drag
Computation 329
13 1 The Jacchia 71 and Jacchia-Bowman 2008 Density Models „unse 329
13 2 The MSIS 2000 Density Model uuesesseseonsnseentssossennonensannsensnnunsuentensennnne
13 3 Two Methods of Determining the Drag Coefficient, Cp
13 3 1 Empirical Curve of Average Cop esccssessssereesesensesses
13 3 2 Theoretical Method Based on Speed Ratio
13 4 Effects and Modeling of CO, Growth in the Upper Atmosphere 338
13 4 1 Simulations Based on Three CO Growth Models csccscecesese 339
13 4 2 Impacts on Fuel Requirements scscsssssoeseeseseceesssceeseneeeeeess 341
13 5 Helium Mismodeling in the NRLMSISE-00 Density Model cssscees 341
13 5 1 Summary of Analysis of Ten Spheres cccssscesseceesesseseeeseseeneee 343
13 52A Proposed Correction Methodology scsssssssscseaseseesseseeassees 344
13 6 Solar Flux and Geomagnetic Index Variations and Forecasting 0 346
13 7, References csccssssssessssesssscssecssssersnescerssesssnsasarsecsesennensscssseuscareneneneenenses 349
Appendix B Solar-Radiation Pressure Perturbation 369
References ccssssssessecsscccsesesssessssscosscsoesesssausvenssusesucseeseusuesseresnansavaneseanesatsneces 386
Appendix C Doubly Averaged Third-Body Gravitational
Perturbation 387
Contents — xiii
Appendix D Simplified Representation of Analytical Long-
Term Equations of Motion for Third-Body
Perturbations 391
Index 397 |
| any_adam_object | 1 |
| author | Chao, Chia-Chun 1939- Hoots, Felix R. 1947- |
| author_GND | (DE-588)1215275773 (DE-588)1215279604 |
| author_facet | Chao, Chia-Chun 1939- Hoots, Felix R. 1947- |
| author_role | aut aut |
| author_sort | Chao, Chia-Chun 1939- |
| author_variant | c c c ccc f r h fr frh |
| building | Verbundindex |
| bvnumber | BV045072604 |
| callnumber-first | T - Technology |
| callnumber-label | TL1080 |
| callnumber-raw | TL1080 |
| callnumber-search | TL1080 |
| callnumber-sort | TL 41080 |
| callnumber-subject | TL - Motor Vehicles and Aeronautics |
| classification_rvk | ZO 8700 |
| ctrlnum | (OCoLC)1193297440 (DE-599)BVBBV045072604 |
| dewey-full | 629.4/113 |
| dewey-hundreds | 600 - Technology (Applied sciences) |
| dewey-ones | 629 - Other branches of engineering |
| dewey-raw | 629.4/113 |
| dewey-search | 629.4/113 |
| dewey-sort | 3629.4 3113 |
| dewey-tens | 620 - Engineering and allied operations |
| discipline | Verkehr / Transport |
| edition | second edition |
| format | Book |
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| id | DE-604.BV045072604 |
| illustrated | Not Illustrated |
| indexdate | 2024-07-31T00:53:57Z |
| institution | BVB |
| isbn | 1884989276 9781884989278 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-030463775 |
| oclc_num | 1193297440 |
| open_access_boolean | |
| owner | DE-83 DE-706 |
| owner_facet | DE-83 DE-706 |
| physical | xviii, 411 Seiten |
| publishDate | 2018 |
| publishDateSearch | 2018 |
| publishDateSort | 2018 |
| publisher | The Aerospace Press American Institute of Aeronautics and Astronautics, Inc. |
| record_format | marc |
| spelling | Chao, Chia-Chun 1939- Verfasser (DE-588)1215275773 aut Applied orbit perturbation and maintenance Chia-Chun "George" Chao and Felix R. Hoots second edition El Segundo, California The Aerospace Press [2018] Reston, Virginia American Institute of Aeronautics and Astronautics, Inc. © 2018 xviii, 411 Seiten txt rdacontent n rdamedia nc rdacarrier Includes bibliographical references and index Artificial satellites Orbits Orbital mechanics Perturbation (Mathematics) Umlaufbahn (DE-588)4238276-2 gnd rswk-swf Satellit (DE-588)4136498-3 gnd rswk-swf Störung (DE-588)4133232-5 gnd rswk-swf Satellit (DE-588)4136498-3 s Umlaufbahn (DE-588)4238276-2 s Störung (DE-588)4133232-5 s DE-604 Hoots, Felix R. 1947- Verfasser (DE-588)1215279604 aut HEBIS Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=030463775&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Chao, Chia-Chun 1939- Hoots, Felix R. 1947- Applied orbit perturbation and maintenance Artificial satellites Orbits Orbital mechanics Perturbation (Mathematics) Umlaufbahn (DE-588)4238276-2 gnd Satellit (DE-588)4136498-3 gnd Störung (DE-588)4133232-5 gnd |
| subject_GND | (DE-588)4238276-2 (DE-588)4136498-3 (DE-588)4133232-5 |
| title | Applied orbit perturbation and maintenance |
| title_auth | Applied orbit perturbation and maintenance |
| title_exact_search | Applied orbit perturbation and maintenance |
| title_full | Applied orbit perturbation and maintenance Chia-Chun "George" Chao and Felix R. Hoots |
| title_fullStr | Applied orbit perturbation and maintenance Chia-Chun "George" Chao and Felix R. Hoots |
| title_full_unstemmed | Applied orbit perturbation and maintenance Chia-Chun "George" Chao and Felix R. Hoots |
| title_short | Applied orbit perturbation and maintenance |
| title_sort | applied orbit perturbation and maintenance |
| topic | Artificial satellites Orbits Orbital mechanics Perturbation (Mathematics) Umlaufbahn (DE-588)4238276-2 gnd Satellit (DE-588)4136498-3 gnd Störung (DE-588)4133232-5 gnd |
| topic_facet | Artificial satellites Orbits Orbital mechanics Perturbation (Mathematics) Umlaufbahn Satellit Störung |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=030463775&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
| work_keys_str_mv | AT chaochiachun appliedorbitperturbationandmaintenance AT hootsfelixr appliedorbitperturbationandmaintenance |