TY - GEN

T1 - Problem of Spacecraft Control by Solar Sail

AU - Polyakhova, E.

AU - Korolev, V .

PY - 2016

Y1 - 2016

N2 - Specificity of motion control of spacecraft with solar sail is determined by the connection of the orbital translation and rotational motions of the whole structure of spacecraft. In order to control the flight, we have to change the size or orientation of the sails. It requires the additional use of energy or fuel costs. The most interesting version of the sail model is that the sail itself would provide control over the correct orientation and maintain the desired position. Stability provides of the moments forces about the center of mass which change the value, if there is a change for small deviations.

AB - Specificity of motion control of spacecraft with solar sail is determined by the connection of the orbital translation and rotational motions of the whole structure of spacecraft. In order to control the flight, we have to change the size or orientation of the sails. It requires the additional use of energy or fuel costs. The most interesting version of the sail model is that the sail itself would provide control over the correct orientation and maintain the desired position. Stability provides of the moments forces about the center of mass which change the value, if there is a change for small deviations.

U2 - DOI: 10.1109/STAB.2016.7541214

DO - DOI: 10.1109/STAB.2016.7541214

M3 - статья в сборнике материалов конференции

SN - ISBN: 978-146739997-5

SP - 7541214

BT - Proceedings of 2016 International Conference "Stability and Oscillations of Nonlinear Control Systems" (Pyatnitskiy's Conference), STAB 2016

A2 - Tkhai, VN

PB - Institute of Electrical and Electronics Engineers Inc.

Y2 - 1 June 2016 through 3 June 2016

ER -