This book consolidates decades of knowledge on space flight navigation
theory, which has thus far been spread across various research articles.
By gathering this research into a single text, it will be more
accessible to students curious about the study of space flight
navigation. Books on optimal control theory and orbital mechanics have
not adequately explored the field of space flight navigation theory
until this point.
The opening chapters introduce essential concepts within optimal control
theory, such as the optimization of static systems, special boundary
conditions, and dynamic equality constraints. An analytical approach is
focused on throughout, as opposed to computational. The result is a book
that emphasizes simplicity and practicability, which makes it accessible
and engaging. This holds true in later chapters that involve orbital
mechanics, two-body maneuvers, bounded inputs, and flight in
non-spherical gravity fields.
The intended audience is primarily upper-undergraduate students,
graduate students, and researchers of aerospace, mechanical, and/or
electrical engineering. It will be especially valuable to those with
interests in spacecraft dynamics and control. Readers should be familiar
with basic dynamics and modern control theory. Additionally, a knowledge
of linear algebra, variational methods, and ordinary differential
equations is recommended.