Fundamentals of astrodynamics (Record no. 2791)
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| 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/> |
| 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 |
