Tkachenko A.I.
Abstract:
The problem of determining attitude of a small spacecraft under conditions, when limitations of energy resources, mass and size of the object force one to refuse controlling its motion with respect to the mass-center. The suggested solution is based on readings of the on-board magnetometer and the familiar from literature means of imitation of solar sensor by comparison of values of electric potential checked on the elements of solar batteries panels. © 2005 by Begell House, Inc.
Author Keywords:
Attitude control; Biaxial magnetometer; Dynamic filtration; Dynamic system; Geomagnetic field; Nanosatellite; Numeric simulation; Observability; Solar sensor; Triaxial magnetometer
Year:
2005
Source title:
Journal of Automation and Information Sciences
Volume:
37
Issue:
8
Page :
58-68
Link:
Scorpus Link
Document Type:
Article
Source:
Scopus
Authors with affiliations:
-
Tkachenko, A.I.
Download Abstract:
geo148.pdf