Cantitate/Preț
Produs

Spacecraft Trajectory Optimization: Cambridge Aerospace Series, cartea 29

Editat de Bruce A. Conway
en Limba Engleză Hardback – 22 aug 2010
This is a long-overdue volume dedicated to space trajectory optimization. Interest in the subject has grown, as space missions of increasing levels of sophistication, complexity, and scientific return - hardly imaginable in the 1960s - have been designed and flown. Although the basic tools of optimization theory remain an accepted canon, there has been a revolution in the manner in which they are applied and in the development of numerical optimization. This volume purposely includes a variety of both analytical and numerical approaches to trajectory optimization. The choice of authors has been guided by the editor's intention to assemble the most expert and active researchers in the various specialities presented. The authors were given considerable freedom to choose their subjects, and although this may yield a somewhat eclectic volume, it also yields chapters written with palpable enthusiasm and relevance to contemporary problems.
Citește tot Restrânge

Toate formatele și edițiile

Toate formatele și edițiile Preț Express
Paperback (1) 32902 lei  6-8 săpt.
  Cambridge University Press – 26 mar 2014 32902 lei  6-8 săpt.
Hardback (1) 91372 lei  6-8 săpt.
  Cambridge University Press – 22 aug 2010 91372 lei  6-8 săpt.

Din seria Cambridge Aerospace Series

Preț: 91372 lei

Preț vechi: 106246 lei
-14% Nou

Puncte Express: 1371

Preț estimativ în valută:
16169 18960$ 14199£

Carte tipărită la comandă

Livrare economică 04-18 februarie 26

Preluare comenzi: 021 569.72.76

Specificații

ISBN-13: 9780521518505
ISBN-10: 0521518504
Pagini: 312
Ilustrații: 77 b/w illus. 29 tables
Dimensiuni: 178 x 254 x 23 mm
Greutate: 0.8 kg
Editura: Cambridge University Press
Colecția Cambridge University Press
Seria Cambridge Aerospace Series

Locul publicării:New York, United States

Cuprins

1. The problem of spacecraft trajectory optimization Bruce A. Conway; 2. Primer vector theory and application John E. Prussing; 3. Spacecraft trajectory optimization using direct transcription and nonlinear programming Stephen W. Paris and Bruce A. Conway; 4. Elements of a software system for spacecraft trajectory optimization Cesar Ocampo; 5. Low-thrust trajectory optimization using orbital averaging and control parameterization Craig A. Kluever; 6. Analytic representation of optimal low-thrust transfer in circular orbit Jean A. Kechichian; 7. Global optimization and space pruning for spacecraft trajectory design Dario Izzo; 8. Incremental techniques for global space trajectory design Massimiliano Vasile and Matteo Ceriotti; 9. Optimal low-thrust trajectories using stable manifolds Christopher Martin and Bruce A. Conway.

Descriere

This volume on space trajectory optimization includes a variety of both analytical and numerical approaches to trajectory optimization.