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Fundamentals of astrodynamics (Record no. 2791)

MARC details
000 -LEADER
fixed length control field 03879cam a2200229 4500
001 - CONTROL NUMBER
control field 3293
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20200722104732.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 710716s1971 nyua b 001 0 eng
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
International Standard Book Number 0486600610
040 ## - CATALOGING SOURCE
Transcribing agency DLC
082 00 - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number 629.4/11
Item number B3285
100 1# - MAIN ENTRY--PERSONAL NAME
Personal name Bate, Roger R.
245 10 - TITLE STATEMENT
Title Fundamentals of astrodynamics
Statement of responsibility, etc / Roger R. Bate, Donald D. Mueller [and] Jerry E. White.
260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT)
Place of publication, distribution, etc New York :
Name of publisher, distributor, etc Dover Publications,
Date of publication, distribution, etc 1971
300 ## - PHYSICAL DESCRIPTION
Extent xii, 455 p.
Other physical details illus.
Dimensions 22 cm.
500 ## - GENERAL NOTE
General note Includes bibliographies.
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name as entry element Astrodynamics.
700 1# - ADDED ENTRY--PERSONAL NAME
Personal name Mueller, Donald D.,
700 1# - ADDED ENTRY--PERSONAL NAME
Personal name White, Jerry E.,
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Koha item type Books
505 0# - FORMATTED CONTENTS NOTE
Formatted contents note Preface<br/>Chapter 1 two-body orbital mechanics<br/>1.1 historical background and basic laws<br/>1.2 the n-body problem<br/>1.3 the two-body problem<br/>1.4 constants of the motion<br/>1.5 the trajectory equation<br/>1.6 relating e and h to the geometry of an orbit<br/>1.7 the elliptical orbit<br/>1.8 the circular orbit<br/>1.9 the parabolic orbit<br/>1.10 the hyperbolic orbit<br/>1.11 canonical units<br/>Exercises<br/>List of references<br/>Chapter 2 orbit determination from observations<br/>2.1 historical background<br/>2.2 coordinate systems<br/>2.3 classical orbital elements<br/>2.4 determining the orbital elements from r and v<br/>2.5 determining r and v from the orbital elements<br/>2.6 coordinate transformations<br/>2.7 orbit determination from a single radar observation<br/>2.8 sez to ijk transformation using an ellipsoid earth model<br/>2.9 the measurement of time<br/>2.10 orbit determination from three position vectors<br/>2.11 orbit determination from optical sightings<br/>2.12 improving a preliminary orbit by differential correction<br/>2.13 space survelliance<br/>2.14 type and location of sensors<br/>2.15 ground track of a satellite<br/>Exercises<br/>List of references<br/>Chapter 3 basic orbital maneuvers<br/>3.1 low altitiude earth orbits<br/>3.2 high altitude earth orbits<br/>3.3 in-plane orbit changes<br/>3.4 out-of-plane orbit changes<br/>Exercises<br/>List of references<br/>Chapter 4 position and velocity as a function of time<br/>4.1 historical background<br/>4.2 time-of-flight as a function of eccentric anomaly<br/>4.3 a universal fomulation for time-of-flight<br/>4.4 the prediction problem<br/>4.5 implementing the universal variable formulation<br/>4.6 classical formulations of the kepler problem<br/>Exercises<br/>List of references<br/>Chapter 5 orbit determination from two positions and time<br/>5.1 historical background<br/>5.2 the gauss problem - general methods of solution<br/>5.3 solution of the gauss problem via universal variables<br/>5.4 the p-iteration method<br/>5.5 the gauss problem using the f and g series<br/>5.6 the original gauss method<br/>5.7 practical applications of the gauss problem - intercept and rendezvous<br/>5.8 determination of orbit from sighting directions at station<br/>Exercises<br/>List of references<br/>Chapter 6 ballistic missile trajectories<br/>6.1 historical background<br/>6.2 the general ballistic missile problem<br/>6.3 effect of launching errors on range<br/>6.4 the effect of earth rotation<br/>Exercises<br/>List of references<br/>Chapter 7 lunar trajectories<br/>7.1 historical background<br/>7.2 the earth-moon system<br/>7.3 simple earth-moon trajectories<br/>7.4 the patched-conic approximation<br/>7.5 non-coplanar lunar trajectories<br/>Exercises<br/>List of references<br/>Chapter 8 interplanetary trajectories<br/>8.1 historical background<br/>8.2 the solar system<br/>8.3 the patched-conic approximation<br/>8.4 non-coplanar interplanetary trajectories<br/>Exercises<br/>List of references<br/>Chapter 9 perturbations<br/>9.1 introduction and historical background<br/>9.2 cowell's method<br/>9.3 encke's method<br/>9.4 variation of parameters or elements<br/>9.5 comments on integration schemes and errors<br/>9.6 numerical integration methods<br/>9.7 analytic formulation of perturbative accelerations<br/>Exercises<br/>List of references<br/>Appendix a astrodynamic constants<br/>Appendix b miscellaneous constants and conversions<br/>Appendix c vector review<br/>Appendix d suggested projects<br/>Index<br/><br/>
Holdings
Withdrawn status Damaged status Not for loan Home library Current library Date acquired Full call number Barcode Date last seen Price effective from Koha item type
      UE-Central Library UE-Central Library 17.07.2018 629.411 B3285 T3293 17.07.2018 17.07.2018 Books
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