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[NT 33762] ISBD
Orbital mechanics for engineering students
[NT 42944] Record Type:
[NT 1579] Language materials, printed : [NT 40817] monographic
[NT 47261] Author:
CurtisHoward D.,
[NT 47351] Place of Publication:
Oxford, UK
[NT 47263] Published:
Elsevier, Butterworth-Heinemann is an imprint of Elsevier;
[NT 47352] Year of Publication:
2014.
[NT 50960] Edition:
3rd ed.
[NT 47264] Description:
xiii, 751 p.ill. : 25 cm.;
[NT 47298] Series:
Elsevier aerospace engineering series
[NT 47266] Subject:
Orbital mechanics. -
[NT 51458] Online resource:
http://www.sciencedirect.com/science/book/9780080977478
[NT 47265] Notes:
Previous edition: 2010.
[NT 50961] ISBN:
9780080977478electronic bk.
[NT 50961] ISBN:
9780080977478
[NT 60779] Content Note:
Dynlmics of point masses The two-body problem Orbital position as a function of time Orbits in three dimensions Preliminary orbit determination Orbital maneuvers Relative motion and rendezvous Interplanetary trajectories Rigid body dynlmics Satellite attitude dynlmics Rocket vehicle dynlmics Introduction to orbital perturbations.
Orbital mechanics for engineering students
Curtis, Howard D.
Orbital mechanics for engineering students
/ Howard D. Curtis, Professor of Aerospace Engineering, Embry-Riddle Aeronautical University, Daytona Beach, Florida. - 3rd ed.. - Oxford, UK : Elsevier, Butterworth-Heinemann is an imprint of Elsevier, 2014.. - xiii, 751 p. ; ill. ; 25 cm.. - (Elsevier aerospace engineering series).
Dynlmics of point masses.
Previous edition: 2010..
Includes bibliographical references (pages 739-740) and index..
ISBN 9780080977478ISBN 9780080977478
Orbital mechanics.
Orbital mechanics for engineering students
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Orbital mechanics for engineering students
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Howard D. Curtis, Professor of Aerospace Engineering, Embry-Riddle Aeronautical University, Daytona Beach, Florida.
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Dynlmics of point masses
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The two-body problem
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Orbital position as a function of time
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Orbits in three dimensions
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Preliminary orbit determination
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Orbital maneuvers
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Relative motion and rendezvous
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Interplanetary trajectories
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Rigid body dynlmics
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Satellite attitude dynlmics
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Rocket vehicle dynlmics
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Introduction to orbital perturbations.
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http://www.sciencedirect.com/science/book/9780080977478
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