Spacecraft navigation and guidance:
Saved in:
| Main Author: | |
|---|---|
| Format: | Book |
| Language: | German |
| Published: |
London [u.a.]
Springer
1998
|
| Series: | Advances in industrial control
|
| Subjects: | |
| Online Access: | Inhaltsverzeichnis |
| Item Description: | Literaturverz. S. 165 - 167. - Auch im Internet unter der Adresse ftp.springer.de in the directory /pub/technik/noton verfügbar |
| Physical Description: | XIV, 181 S. graph. Darst. |
| ISBN: | 3540762485 |
Staff View
MARC
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| 100 | 1 | |a Noton, Maxwell |d 1928- |e Verfasser |0 (DE-588)11805161X |4 aut | |
| 245 | 1 | 0 | |a Spacecraft navigation and guidance |c Maxwell Noton |
| 264 | 1 | |a London [u.a.] |b Springer |c 1998 | |
| 300 | |a XIV, 181 S. |b graph. Darst. | ||
| 336 | |b txt |2 rdacontent | ||
| 337 | |b n |2 rdamedia | ||
| 338 | |b nc |2 rdacarrier | ||
| 490 | 0 | |a Advances in industrial control | |
| 500 | |a Literaturverz. S. 165 - 167. - Auch im Internet unter der Adresse ftp.springer.de in the directory /pub/technik/noton verfügbar | ||
| 650 | 4 | |a Navigation (Astronautics) | |
| 650 | 4 | |a Space vehicles |x Guidance systems | |
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Record in the Search Index
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| adam_text |
CONTENTS
PREFACE
.
IX
1.
ORBITAL
MECHANICS
.
1
1.1
INTRODUCTION
.
1
1.2
THE
TWO-BODY
PROBLEM
.
2
1.3
ORBITAL
ELEMENTS
AND
REFERENCE
AXES
.
4
1.3.1
POSITION
AND
VELOCITY
FROM
THE
ORBITAL
ELEMENTS
.
6
1.3.2
ORBITAL
ELEMENTS
FROM
THE
POSITION
AND
VELOCITY
.
7
1.3.3
NUMERICAL
EXAMPLES
.
8
1.4
TIME
IN
ORBIT
.
9
1.4.1
SOLUTION
FOR
ELLIPSE
.
9
1.4.2
SOLUTION
FOR
HYPERBOLA
.
11
1.4.3
COMPUTATIONS
STARTING
FROM
TIME
IN
ORBIT
.
11
1.5
LAMBERT
'
S
TIME
OF
FLIGHT
THEOREM
.
12
1.6
ORBITAL
MANOEUVRES
.
16
1.6.1
COPLANAR
TRANSFER
MANOEUVRES
.
16
1.6.2
INJECTION
INTO
AN
INTERPLANETARY
ORBIT
.
17
1.6.3
PLANE
CHANGE
TO
INJECT
INTO
A
GEOSTATIONARY
ORBIT
.
19
1.7
PATCHED
CONICS
.
20
1.7.1
SPHERES
OF
INFLUENCE
.
20
1.7.2
TIME
IN
JULIAN
DAYS
.
21
1.7.3
A
SOLAR
POLAR
MISSION
.
22
1.8
NUMERICAL
INTEGRATION
OF
ORBITS
.
25
1.8.1
COWELL
'
S
METHOD
.
25
1.8.2
ENCKE
'
S
METHOD
.
26
1.9
SOFTWARE
.
27
2.
THE
LAUNCH
PHASE
.
29
2.1
INTRODUCTION
.
29
2.2
PROPULSION
.
30
2.2.1
BASICS
.
30
2.2.2
STAGING
.
31
2.3
LAUNCH
SYSTEMS
.
33
2.4
TRAJECTORY
DYNAMICS
.
35
XII
TABLE
OF
CONTENTS
2.4.1
EQUATIONS
OF
MOTION
.
35
2.4.2
GRAVITATIONAL
FORCES
.
38
2.4.3
ROCKET
THRUST
.
39
2.4.4
AERODYNAMIC
FORCES
.
39
2.4.5
FINAL
ORBITAL
ELEMENTS
.
41
2.5
COMPUTATION
OF
THE
NOMINAL
ASCENT
TRAJECTORY
.
41
2.6
A
COMPUTED
EXAMPLE:
ARIANE
4
.
44
2.7
OPTIMIZATION
OF
THE
ASCENT
.
47
2.7.1
SOLUTION
FOR
THE
FLAT
EARTH
.
47
2.7.2
IMPROVEMENT
OF
THE
NOMINAL
TRAJECTORY
.
49
2.8
IN-FLIGHT
GUIDANCE
.
51
2.9
THE
GUIDANCE
AND
NAVIGATION
SYSTEM
.
52
2.10
SOFTWARE
.
54
3.
EARTH
SATELLITES:
PERTURBATIONS
AND
MANOEUVRES
.
55
3.1
INTRODUCTION
.
55
3.2
VARIATION
OF
THE
ORBITAL
ELEMENTS
.
55
3.2.1
RATES
OF
CHANGE
OF
THE
ELEMENTS
.
55
3.2.2
USE
OF
RADIAL
AND
TRANSVERSE
COMPONENTS
.
58
3.2.3
USE
OF
TANGENTIAL
AND
NORMAL
COMPONENTS
.
59
3.2.4
SUMMARY
OF
EQUATIONS
IN
RADIAL-TRANSVERSE
AXES
.
60
3.2.5
SUMMARY
OF
EQUATIONS
IN
TANGENTIAL-NORMAL
AXES.
.
60
3.2.6
EQUATIONS
APPLICABLE
AT
ZERO
ECCENTRICITY
.
60
3.2.7
THE
SINGULARITY
AT
ZERO
INCLINATION
.
61
3.3
GRAVITATIONAL
FIELD
OF
THE
EARTH
.
62
3.3.1
EXPANSION
OF
SPHERICAL
HARMONICS
.
62
3.3.2
EVALUATION
FOR
AN
OBLATE
EARTH
.
63
3.3.3
ANALYTICAL
RESULTS
FOR
AN
OBLATE
EARTH
.
64
3.4
PERTURBATIONS
FROM
THE
SUN
AND
THE
MOON
.
66
3.5
EFFECT
OF ATMOSPHERIC
DRAG
.
67
3.6
ILLUSTRATIVE
COMPUTATIONS
OF
PERTURBATIONS
.
68
3.7
CORRECTING
LOW
EARTH
ORBITS
.
68
3.8
GEOSTATIONARY
ORBITS
.
69
3.8.1
INTRODUCTION
.
69
3.8.2
NORTH-SOUTH
PERTURBATIONS
DUE
TO
THE
MOON
AND
SUN
.
70
3.8.3
EAST-WEST
PERTURBATIONS
DUE
TO
TRIAXIAL
EFFECTS
.
71
3.8.4
EAST-WEST
PERTURBATIONS
DUE
TO
SOLAR
PRESSURE
.
73
3.9
RENDEZVOUS
GUIDANCE
.
75
3.9.1
INTRODUCTION
.
75
3.9.2
GUIDANCE
STRATEGY
.
76
3.9.3
EXAMPLES
BY
SIMULATION
.
77
3.9.4
OTHER
REFERENCES
TO
RENDEZVOUS
AND
DOCKING
.
79
3.10
SOFTWARE
.
80
TABLE
OF
CONTENTS
XIII
4.
ORBIT
DETERMINATION
.
81
4.1
INTRODUCTION
.
81
4.2
FIRST
ESTIMATES
OF
ORBITS
.
83
4.2.1
TRANSFORMATION
TO
OBSERVABLES
.
83
4.2.2
PLANETARY
ORBITS
.
85
4.2.3
COMPUTER
EXAMPLES
OF
PLANETARY
ORBITS
.
87
4.2.4
SPACECRAFT
ORBITS
.
88
4.2.5
COMPUTER
EXAMPLE
OF
EARTH
SATELLITE
.
90
4.3
REFINEMENT
OF
ORBITS
.
90
4.3.1
BATCH
LEAST-SQUARES
FITTING
.
90
4.3.2
GENERATION
OF
PARTIAL
DERIVATIVES
.
92
4.3.3
THE
SQUARE
ROOT
INFORMATION
FILTER
.
93
4.3.4
BIAS
TERMS
AND
THE
CONSIDER
MATRIX
.
96
4.4
SEQUENTIAL
ESTIMATION
.
97
4.4.1
NON-CONSTANT
PARAMETERS
.
97
4.4.2
TIME
UPDATE
WITH
SEQUENTIAL
SRIF
.
98
4.4.3
MEASUREMENT
UPDATE
WITH
SEQUENTIAL
SRIF
.
100
4.4.4
SEQUENTIAL
ESTIMATION
WITH
COVARIANCE
FILTERS
.
100
4.4.5
SRIF
EXAMPLE
WITH
AN
EARTH
SATELLITE
ORBIT
.
101
4.4.6
SRIF
EXAMPLE
FOR
A
SPACECRAFT
APPROACHING
A
COMET
.
104
4.5
SOFTWARE
.
108
5.
MIDCOURSE
AND
GRAVITY
ASSIST
MANOEUVRES
.
109
5.1
INTRODUCTION
.
109
5.2
MIDCOURSE
MANOEUVRES
.
110
5.2.1
NOMINAL
TRAJECTORY
TO
JUPITER
.
110
5.2.2
ERRORS
AT
HELIOCENTRIC
INJECTION
.
ILL
5.2.3
FIXED
TIME
GUIDANCE
.
112
5.2.4
VARIABLE
TIME
GUIDANCE
.
113
5.2.5
PARAMETRIC
RESULTS
.
115
5.3
GRAVITY
ASSIST
MANOEUVRES
.
116
5.3.1
INTRODUCTION
.
116
5.3.2
GRAVITY
ASSIST
IN
TWO
DIMENSIONS
.
118
5.3.3
GRAVITY
ASSIST
IN
THREE
DIMENSIONS
.
119
5.3.4
AN
EXAMPLE
:
COMET
NUCLEUS
SAMPLE
RETURN
.
121
5.4
SOFTWARE
.
123
6.
LOW
THRUST
MISSIONS
.
125
6.1
INTRODUCTION
.
125
6.2
ELECTRIC
PROPULSION
.
125
6.3
OPTIMIZATION
OF
LOW
THRUST
TRAJECTORIES
.
126
6.3.1
OPTIMIZATION
IN
TWO
DIMENSIONS
.
126
6.3.2
PARAMETERIZED
OPTIMIZATION
IN
THREE
DIMENSIONS
.
129
6.3.3
NUMERICAL
EXAMPLE
.
132
6.3.4
CONTROLLABILITY
.
133
XIV
TABLE
OF
CONTENTS
6.4
GUIDANCE
ON
LOW
THRUST
TRAJECTORIES
.
134
6.4.1
INTRODUCTION
.
134
6.4.2
ANALYSIS
.
135
6.4.3
THE
LINEAR
QUADRATIC
CONTROL
PROBLEM
.
136
6.4.4
NUMERICAL
EXAMPLE
OF
FEEDBACK
GUIDANCE
.
137
6.5
SOFTWARE
.
139
7.
ATMOSPHERIC
ENTRY
.
141
7.1
INTRODUCTION
.
141
7.2
FLIGHT
EQUATIONS
.
142
7.2.1
EQUATIONS
OF
MOTION
.
142
7.2.2
AERODYNAMIC
LIFT
AND
DRAG
.
143
7.2.3
HEATING
.
144
7.3
ENTRY
CORRIDORS
.
145
7.3.1
PARAMETERS
.
145
7.3.2
CONDITION
FOR
LEVEL
FLIGHT
.
148
7.3.3
THE
LIMIT
OF
TOTAL
ACCELERATION
.
151
7.3.4
THE
LIMIT
OF
RATE
OF
HEATING
.
151
7.4
BALLISTIC
ENTRY
WITH
NO
LIFT
.
152
7.5
GUIDED
ENTRY
USING
LIFT
.
155
7.5.1
LIFT
AND
THE
GUIDANCE
SYSTEM
.
155
7.5.2
THE
NOMINAL
TRAJECTORY
.
156
7.5.3
FEEDBACK
GUIDANCE
IN
THE
UPPER
ATMOSPHERE
.
158
7.5.4
FEEDBACK
GUIDANCE
IN
THE
LOWER
ATMOSPHERE
.
161
7.6
SOFTWARE
.
164
A.
APPENDICES
.
169
A.L
PERTURBATIONS
FROM
THE
SUN
AND
MOON
IN
GEOSTATIONARY
ORBIT
169
A.
2
PERTURBATIONS
DUE
TO
SOLAR
PRESSURE
IN
GEOSTATIONARY
ORBIT
.
170
A.3
ANGULAR
INFORMATION
FROM
DOPPLER
TRACKING
.
172
A.4
EPHEMERIS
OF
THE
SUN
.
172
A.5
SEQUENTIAL
UD
COVARIANCE
FILTER
.
173
A.6
GLOBAL
POSITIONING
SYSTEM
.
175 |
| any_adam_object | 1 |
| author | Noton, Maxwell 1928- |
| author_GND | (DE-588)11805161X |
| author_facet | Noton, Maxwell 1928- |
| author_role | aut |
| author_sort | Noton, Maxwell 1928- |
| author_variant | m n mn |
| building | Verbundindex |
| bvnumber | BV011814621 |
| callnumber-first | T - Technology |
| callnumber-label | TL1065 |
| callnumber-raw | TL1065 |
| callnumber-search | TL1065 |
| callnumber-sort | TL 41065 |
| callnumber-subject | TL - Motor Vehicles and Aeronautics |
| classification_rvk | US 9500 ZO 8200 |
| classification_tum | VER 840f VER 780f |
| ctrlnum | (OCoLC)246131132 (DE-599)BVBBV011814621 |
| dewey-full | 629.47/42 |
| dewey-hundreds | 600 - Technology (Applied sciences) |
| dewey-ones | 629 - Other branches of engineering |
| dewey-raw | 629.47/42 |
| dewey-search | 629.47/42 |
| dewey-sort | 3629.47 242 |
| dewey-tens | 620 - Engineering and allied operations |
| discipline | Physik Verkehrstechnik Verkehr / Transport |
| format | Book |
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| id | DE-604.BV011814621 |
| illustrated | Illustrated |
| indexdate | 2024-09-10T00:55:15Z |
| institution | BVB |
| isbn | 3540762485 |
| language | German |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-007978194 |
| oclc_num | 246131132 |
| open_access_boolean | |
| owner | DE-91G DE-BY-TUM DE-703 DE-83 |
| owner_facet | DE-91G DE-BY-TUM DE-703 DE-83 |
| physical | XIV, 181 S. graph. Darst. |
| publishDate | 1998 |
| publishDateSearch | 1998 |
| publishDateSort | 1998 |
| publisher | Springer |
| record_format | marc |
| series2 | Advances in industrial control |
| spelling | Noton, Maxwell 1928- Verfasser (DE-588)11805161X aut Spacecraft navigation and guidance Maxwell Noton London [u.a.] Springer 1998 XIV, 181 S. graph. Darst. txt rdacontent n rdamedia nc rdacarrier Advances in industrial control Literaturverz. S. 165 - 167. - Auch im Internet unter der Adresse ftp.springer.de in the directory /pub/technik/noton verfügbar Navigation (Astronautics) Space vehicles Guidance systems Bahnsteuerung (DE-588)4042803-5 gnd rswk-swf Raumfahrzeug (DE-588)4048579-1 gnd rswk-swf Raumflugbahn (DE-588)4177065-1 gnd rswk-swf Raumfahrzeug (DE-588)4048579-1 s Raumflugbahn (DE-588)4177065-1 s Bahnsteuerung (DE-588)4042803-5 s DE-604 DNB Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=007978194&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Noton, Maxwell 1928- Spacecraft navigation and guidance Navigation (Astronautics) Space vehicles Guidance systems Bahnsteuerung (DE-588)4042803-5 gnd Raumfahrzeug (DE-588)4048579-1 gnd Raumflugbahn (DE-588)4177065-1 gnd |
| subject_GND | (DE-588)4042803-5 (DE-588)4048579-1 (DE-588)4177065-1 |
| title | Spacecraft navigation and guidance |
| title_auth | Spacecraft navigation and guidance |
| title_exact_search | Spacecraft navigation and guidance |
| title_full | Spacecraft navigation and guidance Maxwell Noton |
| title_fullStr | Spacecraft navigation and guidance Maxwell Noton |
| title_full_unstemmed | Spacecraft navigation and guidance Maxwell Noton |
| title_short | Spacecraft navigation and guidance |
| title_sort | spacecraft navigation and guidance |
| topic | Navigation (Astronautics) Space vehicles Guidance systems Bahnsteuerung (DE-588)4042803-5 gnd Raumfahrzeug (DE-588)4048579-1 gnd Raumflugbahn (DE-588)4177065-1 gnd |
| topic_facet | Navigation (Astronautics) Space vehicles Guidance systems Bahnsteuerung Raumfahrzeug Raumflugbahn |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=007978194&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
| work_keys_str_mv | AT notonmaxwell spacecraftnavigationandguidance |