Abstract
Using the methods of Chapters 1–4, we study to a first approximation problems of the optimal control of plane orbital motions of spacecrafts. We consider also problems of the optimal and suboptimal control of spacecraft rotation relative to its centre of mass, in particular, stabilization problems.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
Author information
Authors and Affiliations
Rights and permissions
Copyright information
© 1994 Springer Science+Business Media Dordrecht
About this chapter
Cite this chapter
Akulenko, L.D. (1994). Optimal Control of Orbital Motions and Rotations of Spacecrafts Using “Low Thrust”. In: Problems and Methods of Optimal Control. Mathematics and Its Applications, vol 286. Springer, Dordrecht. https://doi.org/10.1007/978-94-011-1194-2_6
Download citation
DOI: https://doi.org/10.1007/978-94-011-1194-2_6
Publisher Name: Springer, Dordrecht
Print ISBN: 978-94-010-4522-3
Online ISBN: 978-94-011-1194-2
eBook Packages: Springer Book Archive