Lunar transfer orbits utilizing solar perturbations and ballistic capture:
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
München
Utz, Wiss.
2002
|
| Schlagworte: | |
| Online-Zugang: | Inhaltsverzeichnis |
| Beschreibung: | Zugl.: München, Techn. Univ., Diss., 2002 |
| Beschreibung: | V, 178 S. graph. Darst. : 21 cm |
| ISBN: | 3831601550 |
Internformat
MARC
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|---|---|---|---|
| 001 | BV014670572 | ||
| 003 | DE-604 | ||
| 005 | 20030121 | ||
| 007 | t | ||
| 008 | 020820s2002 gw d||| m||| 00||| eng d | ||
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| 020 | |a 3831601550 |9 3-8316-0155-0 | ||
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| 100 | 1 | |a Seefelder, Wolfgang |e Verfasser |4 aut | |
| 245 | 1 | 0 | |a Lunar transfer orbits utilizing solar perturbations and ballistic capture |c Wolfgang Seefelder |
| 264 | 1 | |a München |b Utz, Wiss. |c 2002 | |
| 300 | |a V, 178 S. |b graph. Darst. : 21 cm | ||
| 336 | |b txt |2 rdacontent | ||
| 337 | |b n |2 rdamedia | ||
| 338 | |b nc |2 rdacarrier | ||
| 500 | |a Zugl.: München, Techn. Univ., Diss., 2002 | ||
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| 883 | 1 | |8 1\p |a cgwrk |d 20201028 |q DE-101 |u https://d-nb.info/provenance/plan#cgwrk | |
| 943 | 1 | |a oai:aleph.bib-bvb.de:BVB01-009953148 | |
Datensatz im Suchindex
| _version_ | 1808226715260944384 |
|---|---|
| adam_text |
CONTENTS
PREFACE
I
1
INTRODUCTION
1
2
FUNDAMENTALS
OF
ASTRODYNAMICS
5
2.1
TIME
.
5
2.1.1
SIDEREAL
TIME
.
6
2.1.2
SOLAR
AND
UNIVERSAL
TIME
.
7
2.1.3
DYNAMICAL
TIME
.
8
2.1.4
ATOMIC
TIME
.
8
2.2
COORDINATE
SYSTEMS
.
9
2.2.1
GEOCENTRIC
EQUATORIAL
COORDINATE
SYSTEM
.
10
2.2.2
MOON
CENTERED
EQUATORIAL
COORDINATE
SYSTEM
.
10
2.2.3
PERIFOCAL
COORDINATE
SYSTEM
.
12
2.2.4
CLASSICAL
ORBITAL
ELEMENTS
.
13
2.2.5
COORDINATE
TRANSFORMATIONS
.
14
2.3
EQUATIONS
OF
MOTION
.
10
2.3.1
THE
N-BODY
PROBLEM
.
17
2.3.2
THE
RESTRICTED
TWO-BODY
PROBLEM
.
19
2.4
SPECIAL
PERTURBATION
TECHNIQUES
.
24
2.4.1
GRAVITY
FIELD
OF
A
CENTRAL
BODY
.
25
2.4.2
THIRD-BODY
PERTURBATIONS
.
27
2.4.3
ATMOSPHERIC
DRAG
.
28
2.4.4
SOLAR
RADIATION
PRESSURE
.
29
2.5
NUMERICAL
INTEGRATION
METHODS
.
30
IV
CONTENTS
2.6
NUMERICAL
OPTIMIZATION
METHODS
.
33
3
ORBITAL
TRANSFER
37
3.1
MISSION
CONSTRAINTS
.
37
3.1.1
MOTION
OF
THE
MOON
.
38
3.1.2
LUNAR
ORBIT
.
39
3.1.3
STANDARD
ARIANE
5
GEOSTATIONARY
TYANSFER
ORBIT
.
40
3.2
TANGENTIAL
ORBITAL
TRANSFER
.
40
3.2.1
COPLANAR
TRANSFER
ORBITS
.
40
3.2.2
NON-COPLANAR
TRANSFER
ORBITS
.
43
3.3
CIRCULAR
RESTRICTED
THREE-BODY
PROBLEM
.
47
3.4
LOW
ENERGY
TRANSFERS
BETWEEN
THE
EARTH
AND
THE
MOON
.
51
3.5
SUMMARY
.
58
4
LINEAR
ORBIT
THEORY
61
4.1
INTRODUCTION
.
61
4.2
LINEARIZATION
OF
THE
EQUATIONS
OF
MOTION
.
61
4.3
EFFECTS
OF
THE
SOLAR
GRAVITY
GRADIENT
.
65
4.3.1
PERICENTER-RAISE
MANEUVER
.
65
4.3.2
INCLINATION-ONLY
CHANGE
MANEUVER
.
67
4.3.3
PROJECTED
ACCELERATION
DUE
TO
THE
SOLAR
GRAVITY
GRADIENT
.
68
4.3.4
MAGNITUDE
OF
VELOCITY
CHANGE
.
75
4.3.5
MAGNITUDE
OF
INCLINATION
CHANGE
.
83
4.3.6
IMPLICATIONS
ON
THE
EARTH-MOON-SUN
CONFIGURATION
AT
ARRIVAL
.
84
4.4
SUMMARY
.
85
5
THEORY
AND
NUMERICAL
MODEL
VERIFICATION
87
5.1
HITEN
-
FIRST
WSB
TRANSFER
.
87
5.1.1
MISSION
DESCRIPTION
.
87
5.1.2
THEORETICAL
ANALYSIS
AND
NUMERICAL
REPRODUCTION
.
89
5.2
NOZOMI
-
MISSION
TO
MARS
.
93
5.2.1
MISSION
DESCRIPTION
.
93
5.2.2
THEORETICAL
ANALYSIS
AND
NUMERICAL
REPRODUCTION
.
95
CONTENTS
V
6
SUN
PERTURBED
LUNAR
TRANSFER
101
6.1
STEPWISE
APPROACH
PHILOSOPHY
.
102
6.2
COMPUTATION
AND
OPTIMIZATION
STRATEGY
.
104
6.2.1
PARAMETERIZATION
OF
THE
TRANSFER
PROBLEM
.
104
6.2.2
SOLVING
LAMBERT
'
S
PROBLEM
.
105
6.2.3
SOLVING
KEPLER'S
PROBLEM
.
107
6.2.4
FORCE
MODEL
FOR
NUMERICAL
INTEGRATION
.
109
6.3
COMPUTATION
RESULTS
.
110
6.3.1
PATCHED
CONICS
APPROXIMATION
.
ILL
6.3.2
NUMERICAL
INTEGRATION
.
119
6.4
VISUALIZATION
OF
SAMPLE
TRANSFERS
.
127
6.5
DISCUSSION
OF
RESULTS
AND
SUMMARY
.
130
7
BALLISTIC
CAPTURE
TRANSFER
133
7.1
OPTIMIZATION
STRATEGY
AND
ALGORITHM
.
134
7.1.1
STEPWISE
APPROACH
PHILOSOPHY
.
134
7.1.2
PARAMETERIZATION
OF
THE
TRANSFER
PROBLEM
.
136
7.1.3
FORCE
MODEL
FOR
NUMERICAL
INTEGRATION
.
139
7.1.4
BISECTION
ROOT
FINDER
.
139
7.2
RESULTS
-
BIFURCATION
SCAN
.
140
7.3
RESULTS
-
OPTIMIZED
TRANSFER
SAMPLES
.
145
7.4
DISCASSION
AND
SUMMARY
.
163
8
SUMMARY
167
A
LIST
OF
SYMBOLS
169
B
LIST
OF
ACRONYMS
173
REFERENCES
174 |
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| discipline | Verkehrstechnik |
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| genre_facet | Hochschulschrift |
| geographic | Sonne (DE-588)1236963652 gnd |
| geographic_facet | Sonne |
| id | DE-604.BV014670572 |
| illustrated | Illustrated |
| indexdate | 2024-08-24T00:29:35Z |
| institution | BVB |
| isbn | 3831601550 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-009953148 |
| oclc_num | 53289063 |
| open_access_boolean | |
| owner | DE-12 DE-91G DE-BY-TUM DE-706 |
| owner_facet | DE-12 DE-91G DE-BY-TUM DE-706 |
| physical | V, 178 S. graph. Darst. : 21 cm |
| publishDate | 2002 |
| publishDateSearch | 2002 |
| publishDateSort | 2002 |
| publisher | Utz, Wiss. |
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| spelling | Seefelder, Wolfgang Verfasser aut Lunar transfer orbits utilizing solar perturbations and ballistic capture Wolfgang Seefelder München Utz, Wiss. 2002 V, 178 S. graph. Darst. : 21 cm txt rdacontent n rdamedia nc rdacarrier Zugl.: München, Techn. Univ., Diss., 2002 Raumflugbahn (DE-588)4177065-1 gnd rswk-swf Trajektorie Kinematik (DE-588)4208631-0 gnd rswk-swf Mondflug (DE-588)4170433-2 gnd rswk-swf Störung (DE-588)4133232-5 gnd rswk-swf Sonne (DE-588)1236963652 gnd rswk-swf (DE-588)4113937-9 Hochschulschrift gnd-content Mondflug (DE-588)4170433-2 s Trajektorie Kinematik (DE-588)4208631-0 s DE-604 Raumflugbahn (DE-588)4177065-1 s Störung (DE-588)4133232-5 s Sonne (DE-588)1236963652 g 1\p DE-604 DNB Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=009953148&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 | Seefelder, Wolfgang Lunar transfer orbits utilizing solar perturbations and ballistic capture Raumflugbahn (DE-588)4177065-1 gnd Trajektorie Kinematik (DE-588)4208631-0 gnd Mondflug (DE-588)4170433-2 gnd Störung (DE-588)4133232-5 gnd |
| subject_GND | (DE-588)4177065-1 (DE-588)4208631-0 (DE-588)4170433-2 (DE-588)4133232-5 (DE-588)1236963652 (DE-588)4113937-9 |
| title | Lunar transfer orbits utilizing solar perturbations and ballistic capture |
| title_auth | Lunar transfer orbits utilizing solar perturbations and ballistic capture |
| title_exact_search | Lunar transfer orbits utilizing solar perturbations and ballistic capture |
| title_full | Lunar transfer orbits utilizing solar perturbations and ballistic capture Wolfgang Seefelder |
| title_fullStr | Lunar transfer orbits utilizing solar perturbations and ballistic capture Wolfgang Seefelder |
| title_full_unstemmed | Lunar transfer orbits utilizing solar perturbations and ballistic capture Wolfgang Seefelder |
| title_short | Lunar transfer orbits utilizing solar perturbations and ballistic capture |
| title_sort | lunar transfer orbits utilizing solar perturbations and ballistic capture |
| topic | Raumflugbahn (DE-588)4177065-1 gnd Trajektorie Kinematik (DE-588)4208631-0 gnd Mondflug (DE-588)4170433-2 gnd Störung (DE-588)4133232-5 gnd |
| topic_facet | Raumflugbahn Trajektorie Kinematik Mondflug Störung Sonne Hochschulschrift |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=009953148&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
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