Fundamentals of Astrodynamics and Applications

Portada
Springer Science & Business Media, 2001 M06 30 - 958 páginas

Fundamentals of Astrodynamics and Applications is rapidly becoming the standard astrodynamics reference for those involved in the business of spaceflight. What sets this book apart is that nearly all of the theoretical mathematics is followed by discussions of practical applications implemented in tested software routines. For example, the book includes a compendium of algorithms that allow students and professionals to determine orbits with high precision using a PC. Without a doubt, when an astrodynamics problem arises in the future, it will become standard practice for engineers to keep this volume close at hand and `look it up in Vallado'.
While the first edition was an exceptionally useful and popular book throughout the community, there are a number of reasons why the second edition will be even more so. There are many reworked examples and derivations. Newly introduced topics include ground illumination calculations, Moon rise and set, and a listing of relevant Internet sites. There is an improved and expanded discussion of coordinate systems, orbit determination, and differential correction. Perhaps most important is that all of the software routines described in the book are now available for free in FORTRAN, PASCAL, and C. This makes the second edition an even more valuable text and superb reference.

 

Contenido

CHAPTER 1 EQUATIONS OF MOTION
1
Ellipse
13
a r p
16
100
17
140
18
1P
19
A
21
fpat
25
Interceptor t
394
CHAPTER 7
403
Λ
436
D N W
438
F
450
Tigt b
473
Short way Av 180
474
tgt
475

T
46
CHAPTER 2
49
dr
67
K
88
1 16609U 86017A 9335253502934 00007889 000000 105293
115
Notice that A is the only fast variable In
117
we can elegantly work around this limitation We can
123
orbit in space in three dimensions we can fix
127
CHAPTER 3
135
f 15 e 06
141
K
153
K
163
0
166
Earth
181
CHAPTER 4
235
IF Elevation 90
255
CHAPTER 5
265
New
283
Star
301
Problems
304
CHAPTER 6
305
Final
309
2μ a initial
317
Initial
330
ΔΩ
337
Initial orbit
339
Phasing orbit
348
K
354
tgt
375
CHAPTER 8
491
ical location of the third body Thus they
545
CHAPTER 9
567
Σ
587
K
600
Apogee Start
619
Short periodic
621
Resonance is the appearance of unusual longperiodic contributions
623
II
628
spheric density are greatest the energy drain is also
634
CHAPTER 10
675
are available Doppler measurement errors are a function
685
P
688
Xk1k
721
Kalman FilterLinear System
729
observations from the state X Notice the use
735
CHAPTER 11
769
Phorizon
783
î
795
lites in six orbital planes with four satellites in
820
Apogee
842
want to create this region so the major axis is
844
APPENDIX A
853
APPENDIX B
867
APPENDIX C
883
APPENDIX D
905
The numbers in brackets after each reference indicate the chapter
929
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