In this chapter we develop a general theory of optimal spacecraft trajectories based on two pioneering works: Breakwell [1959] and Lawden [1963]. Lawden introduced the concept of the primer vector, which plays a dominant role in minimum-propellant trajectories and also in other types of optimal trajectories. A more complete discussion of the topics in this chapter, including several example trajectories, is in Prussing [2010].
General Theory of Optimal Rocket Trajectories
Space Technology Library
18.09.2013
20 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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