Interplanetary Astrodynamics

This book covers the orbital mechanics tools and techniques necessary to design, predict, and guide a trajectory of a spacecraft traveling between two or more bodies in a Solar System. It emphasizes the interplanetary aspects of space missions and is written for instructors, graduate students, and advanced undergraduate students in Aerospace and Mechanical Engineering.

Format: Hardback
Length: 386 pages
Publication date: 28 April 2023
Publisher: Taylor & Francis Ltd

Focusing on the orbital mechanics tools and techniques necessary to design, predict, and guide a trajectory of a spacecraft traveling between two or more bodies in a Solar System, this comprehensive book delves into the dynamical theory required to describe the motion of bodies in space. It examines the N-body problem, a fundamental challenge in celestial mechanics, and showcases its applications in designing interplanetary missions. While most orbital mechanics books primarily address Earth-orbiting spacecraft with a brief discussion of interplanetary missions, this book takes a unique approach by emphasizing the interplanetary aspects of space missions. Written with instructors, graduate students, and advanced undergraduate students in Aerospace and Mechanical Engineering in mind, this book offers in-depth explanations of interplanetary trajectory design, navigation, and targeting.

The book begins by introducing the fundamental principles of orbital mechanics, including Kepler's laws of planetary motion and Newton's laws of motion. It then explores the concept of angular momentum, a crucial parameter in determining the motion of celestial bodies. The authors discuss the application of orbital mechanics to the design of spacecraft trajectories, including the use of orbital elements such as eccentricity, inclination, and longitude of the ascending node.

Next, the book delves into the N-body problem, a complex mathematical model that describes the motion of multiple interacting bodies in space. It discusses the methods used to solve the N-body problem, including numerical integration and analytical solutions. The authors illustrate the application of the N-body problem to the design of interplanetary missions, such as the Mars Exploration Rovers and the Voyager spacecraft.

Throughout the book, real-world examples and case studies are used to demonstrate the practical applications of orbital mechanics. These examples cover a wide range of space missions, including the Apollo Moon landings, the Space Shuttle program, and the Mars Exploration Rovers. The authors use these examples to highlight the challenges and opportunities associated with interplanetary space travel and to illustrate the importance of accurate trajectory design and navigation.

In conclusion, this book is an essential resource for instructors, graduate students, and advanced undergraduate students in Aerospace and Mechanical Engineering. It provides a comprehensive and up-to-date introduction to the dynamical theory of orbital mechanics, the N-body problem, and their applications in interplanetary trajectory design, navigation, and targeting. With its clear and concise writing style, real-world examples, and comprehensive coverage, this book is sure to be a valuable tool for anyone interested in space exploration and the future of humanity's space endeavors.

Weight: 706g
Dimension: 240 x 165 x 28 (mm)
ISBN-13: 9780367759704