Journal of Automation and Information Sciences
Выходит 12 номеров в год
ISSN Печать: 1064-2315
ISSN Онлайн: 2163-9337
SJR:
0.173
SNIP:
0.588
CiteScore™::
2
Indexed in
Optimal Fuel Expenditure Control of the Angular Attitude of a Spacecraft
Том 30,
Выпуск 4-5, 1998,
pp. 193-202
DOI: 10.1615/JAutomatInfScien.v30.i4-5.210
Краткое описание
A control (optimal in the sense of the time-optimal fuel expenditure) problem of the angular altitude (stabilization) of a spacecraft is considered in the continuous- as well as in discrete-time statement. The synthesis of an optimal control algorithm for chosen performance indices is carried out on the base of the minimum principle and reachable sets that are constructed in the plane of the turn angles and on whose boundaries switchings of the optimal control are realized. An analysis of the results obtained is performed, which allows one to find a one-to-one correspondence between the duration of the optimal steering and a given turn angle of the spacecraft.
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Index, Volume 52, 2020