Preliminary Design of Spacecraft Trajectories for Missions to Outer Planets and Small Bodies
Author: Demyan Vasilyevich Lantukh
Publisher:
Published: 2015
Total Pages: 510
ISBN-13:
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Author: Demyan Vasilyevich Lantukh
Publisher:
Published: 2015
Total Pages: 510
ISBN-13:
DOWNLOAD EBOOKAuthor: Wang Sang Koon
Publisher: Springer
Published: 2011-06-01
Total Pages: 336
ISBN-13: 9780387495156
DOWNLOAD EBOOKThis book considers global solutions to the restricted three-body problem from a geometric point of view. The authors seek dynamical channels in the phase space which wind around the planets and moons and naturally connect them. These low energy passageways could slash the amount of fuel spacecraft need to explore and develop our solar system. In order to effectively exploit these passageways, the book addresses the global transport. It goes beyond the traditional scope of libration point mission design, developing tools for the design of trajectories which take full advantage of natural three or more body dynamics, thereby saving precious fuel and gaining flexibility in mission planning. This is the key for the development of some NASA mission trajectories, such as low energy libration point orbit missions (e.g., the sample return Genesis Discovery Mission), low energy lunar missions and low energy tours of outer planet moon systems, such as a mission to tour and explore in detail the icy moons of Jupiter. This book can serve as a valuable resource for graduate students and advanced undergraduates in applied mathematics and aerospace engineering, as well as a manual for practitioners who work on libration point and deep space missions in industry and at government laboratories. the authors include a wealth of background material, but also bring the reader up to a portion of the research frontier.
Author: Donald Hamilton Ellison
Publisher:
Published: 2018
Total Pages:
ISBN-13:
DOWNLOAD EBOOKAuthor: OV Papkov
Publisher: Routledge
Published: 2017-11-01
Total Pages: 296
ISBN-13: 1351429701
DOWNLOAD EBOOKReflecting the results of twenty years; experience in the field of multipurpose flights, this monograph includes the complex routes of the trajectories of a number of bodies (e.g., space vehicles, comets) in the solar system. A general methodological approach to the research of flight schemes and the choice of optimal performances is developed. Additionally, a number of interconnected methods and algorithms used at sequential stages of such development are introduced, which allow the selection of a rational multipurpose route for a space vehicle, the design of multipurpose orbits, the determination of optimal space vehicle design, and ballistic performances for carrying out the routes chosen. Other topics include the practical results obtained from using these methods, navigation problems, near-to-planet orbits, and an overview of proven and new flight schemes.
Author: Paolo De Pascale (; Roma>)
Publisher:
Published: 2007
Total Pages:
ISBN-13:
DOWNLOAD EBOOKAuthor: John D. McLean
Publisher:
Published: 1971
Total Pages: 100
ISBN-13:
DOWNLOAD EBOOKThis report cicals with the problcm of determining the trajectory of a spacecraft from on-board optical measurents without a priori information. Only sufficient information to determine the trajectory is used, and it is assumed that this preliminary estimate will be improved later by the use of differential corrections and redundant data. Five basic types of measurements, representing instruments considered feasible or within the state of the art, are considered. The effects of random and bias type measurement errors and interpolation errors arising from nonsimultaneous measurements are analyzed. Only observations of the central body and two stars are considered. Within certain limitations all five types of measurements will give satisfactory results. Two important factors discussed in the report are the proper choice of stars and the calibration for eliminating bias errors.
Author: Synthia Mirlin Findlay
Publisher:
Published: 2006
Total Pages: 180
ISBN-13:
DOWNLOAD EBOOKAuthor: James Miller
Publisher: Springer
Published: 2018-09-03
Total Pages: 395
ISBN-13: 3319789163
DOWNLOAD EBOOKThis textbook introduces the theories and practical procedures used in planetary spacecraft navigation. Written by a former member of NASA's Jet Propulsion Laboratory (JPL) navigation team, it delves into the mathematics behind modern digital navigation programs, as well as the numerous technological resources used by JPL as a key player in the field. In addition, the text offers an analysis of navigation theory application in recent missions, with the goal of showing students the relationship between navigation theory and the real-world orchestration of mission operations.
Author: John E. Prussing
Publisher: Oxford University Press
Published: 2018
Total Pages: 151
ISBN-13: 019881108X
DOWNLOAD EBOOKA textbook on the theory and applications of optimal spacecraft trajectories
Author: Jeffrey S. Parker
Publisher: John Wiley & Sons
Published: 2014-06-25
Total Pages: 452
ISBN-13: 1118855310
DOWNLOAD EBOOKBased on years of research conducted at the NASA Jet Propulsion Laboratory, Low-Energy Lunar Trajectory Design provides high-level information to mission managers and detailed information to mission designers about low-energy transfers between Earth and the moon. The book answers high-level questions about the availability and performance of such transfers in any given month and year. Low-energy lunar transfers are compared with various other types of transfers, and placed within the context of historical missions. Using this book, designers may reconstruct any transfer described therein, as well as design similar transfers with particular design parameters. An Appendix, “Locating the Lagrange Points,” and a useful list of terms and constants completes this technical reference. Surveys thousands of possible trajectories that may be used to transfer spacecraft between Earth and the moon, including transfers to lunar libration orbits, low lunar orbits, and the lunar surface Provides information about the methods, models, and tools used to design low-energy lunar transfers Includes discussion about the variations of these transfers from one month to the next, and the important operational aspects of implementing a low-energy lunar transfer Additional discussions address navigation, station-keeping, and spacecraft systems issues