An obvious alternative to the coning maneuver is to use thrusters RCS-3 and 4 to despin the craft completely, thrusters RCS-5 and 6 to initiate roll around the y axis and stop it after 90◦, and then RCS-3 and 4 to respin the spacecraft ...
Reference 7 presents an analysis that optimizes the plane change distribution among the three AVs and optimizes the intermediate apogee radius to minimize the total AV for a specified ratio of final to initial orbit radii and for a ...
Completely revised and updated, this edition provides: * Current data and statistics, along with coverage of new research and the most recent developments in the field * Three new chapters: "The Three-Body Problem" (Ch. 4), "Continuous ...
A lively study of orbital mechanics by the writer responsible for the computer simulations and systems analysis for the Saturn V moon rocket, Project Skylab and many others.
Designed to be used as a graduate student textbook and a ready reference for the busy professional, Orbital Mechanics, Second Edition is structured so that you can easily look up...
Although its aim is to provide the engineer and scientist with a concise treatment of the basic elements of orbital mechanics, this book should also be suitable for senior undergraduate and graduate courses.