1996. First Edition. Hardcover. Discusses some techniques used to obtain numerical solutions of the equations of motion for planets and satellites. This book also introduces the two-body problem and solves it by developing six integrals of the motion, starting from Newton's three laws of motion and his law of gravitation and then using vector algebra to develop the integrals. Num Pages: 264 pages, 10 tables, 50 halftones. BIC Classification: PHVB; TTDS. Category: (P) Professional & Vocational; (U) Tertiary Education (US: College). Dimension: 229 x 152 x 15. Weight in Grams: 542. . . . . . Books ship from the US and Ireland.

N� de ref. del art�culo V9780691044590

Contactar al vendedor

Denunciar este art�culo

Detalles bibliogr�ficos

T�tulo: Modern Astrodynamics: Fundamentals and Perturbation Methods
Editor: Princeton University Press
Fecha de publicaci�n: 1996
Idioma: Ingl�s
ISBN 10: 0691044597
ISBN 13: 9780691044590
Encuadernaci�n: Encuadernaci�n de tapa dura
Estado: New

Acerca de

Sinopsis

Newton’s laws of motion and his universal law of gravitation described mathematically the motion of two bodies undergoing mutual gravitational attraction. However, it is impossible to solve analytically the equation of motion for three gravitationally interacting bodies. This book discusses some techniques used to obtain numerical solutions of the equations of motion for planets and satellites, which are of fundamental importance to solar-system dynamicists and to those involved in planning the orbits of artificial satellites.

The first part introduces the classical two-body problem and solves it by rigorously developing the six integrals of the motion, starting from Newton’s three laws of motion and his law of gravitation and then using vector algebra to develop the integrals. The various forms of the solution flow naturally from the integrals. In the second part, several modern perturbation techniques are developed and applied to cases of practical importance. For example, the perturbed two-body problem for an oblate planet or for a nonsymmetric rotating planet is considered, as is the effect of drag on a satellite. The two-body problem is regularized, and the nonlinear differential equation is thereby transformed to a linear one by further embedding several of the integrals. Finally, a brief sketch of numerical methods is given, as the perturbation equations must be solved by numerical rather than by analytical methods.

Acerca del autor

Victor R. Bond and Mark C. Allman are Senior Engineers for McDonnell Douglas Space Science Corporation.

"Sobre este t�tulo" puede pertenecer a otra edici�n de este libro.

Descripci�n de la librer�a

We carry a comprehensive range of out of print and rare books.

Ver la p�gina web de la librer�a

Informaci�n empresarial del vendedor

Kennys Bookshops and Art Galleries Limited
Liosban Industrial Estate, Tuam Road, Galway, GY, Ireland

Condiciones de venta y env�o

Condiciones de venta

We guarantee the condition of every book as it's described on the Abebooks websites.

If you're dissatisfied with your purchase (Incorrect Book/Not as Described/Damaged) or if the order hasn't arrived, you're eligible for a refund within 30 days of the estimated delivery date.

For any queries please use the contact seller link or send an email to books@kennys.ie

Conor Kenny

Derecho a cancelaci�n

Condiciones de env�o

All books securely packaged. Some books ship from Ireland.

Tarifas de env�o en Estados Unidos de America

Tarifas de env�o en Estados Unidos de America
Cantidad del pedido	De 14 a 20 d�as h�biles	De 13 a 14 d�as h�biles
Primer art�culo	EUR 9.01	EUR 18.02

Los plazos de entrega los establecen los vendedores y var�an seg�n el transportista y la ubicaci�n. Los pedidos que pasan por la aduana pueden sufrir retrasos y los compradores son responsables de los aranceles o tarifas asociadas. Los vendedores pueden ponerse en contacto con usted en relaci�n con cargos adicionales para cubrir cualquier aumento en los costes de env�o de los art�culos.