NDLI: Synthesis of spacecraft covariance controls

Content Provider	Springer Nature Link
Author	Zubov, N. E. Misrikhav, M. Sh. Ryabchenko, V. N.
Copyright Year	2014
Abstract	For a linear multidimensional mathematical model of spacecraft motion, a method for designing a highly accurate feedback for the spacecraft control system is developed. The proposed method is based on the relationship between the modal, optimizing, and covariance approaches to the feedback synthesis aimed at satisfying the prescribed requirements for the spacecraft control quality; this relationship is established in the paper. An example of the application of the proposed approach to the orbital stabilization of a spacecraft is discussed and simulation results are presented.
Starting Page	925
Ending Page	938
Page Count	14
File Format	PDF
ISSN	10642307
Journal	Journal of Computer and Systems Sciences International
Volume Number	53
Issue Number	6
e-ISSN	15556530
Language	English
Publisher	Pleiades Publishing
Publisher Date	2014-12-03
Publisher Place	Moscow
Access Restriction	One Nation One Subscription (ONOS)
Subject Keyword	Control, Robotics, Mechatronics
Content Type	Text
Resource Type	Article
Subject	Applied Mathematics Theoretical Computer Science Computer Networks and Communications Control and Systems Engineering Information Systems Computer Vision and Pattern Recognition Software

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Synthesis of spacecraft covariance controls