Most space systems can be considered as a system of rigid bodies, and in some cases, with additional elastic and viscoelastic elements and fuel residuals. Rigid Body Dynamics for Space Applications shows the nature of the phenomena and explains the behavior of space objects.
The book covers modern problems of spaceflight mechanics, such as attitude dynamics of re-entry and space debris in Earth's atmosphere; dynamics and control of coaxial satellite gyrostats; deployment, dynamics and control of a tether-assisted return mission of a re-entry capsule; and removal of large space debris by a tether tow. Researchers working on spacecraft attitude dynamics or space debris removal as well as those in the fields of mechanics, aerospace engineering and aerospace science will benefit from this book.
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