The thermal analysis of spacecrafts with orientation and geometric configuration varying during an orbit revolution. New software version

1Kislov, AM, 1Romanenko, VG, 1Fenchenko, VN
1B.Verkin Institute for Low Temperature Physics and Engineering of the National Academy of Sciences of Ukraine, Kharkiv, Ukraine
Kosm. nauka tehnol. 2012, 18 ;(1):21–30
https://doi.org/10.15407/knit2012.01.021
Section: Spacecraft Dynamics and Control
Publication Language: Russian
Abstract: 
We describe a procedure for taking into account the satellite orientation inaccuracy during shooting with nonzero angular velocity with the use of remote sensing satellites and highspatialresolution optical-electronic scanners. We give some results of computer simulation of complex deskside territory shooting with a software control of the satellite orientation in the course of shooting.
Keywords: modeling, thermal modes of a spacecraft
References: 
1. Gavrilov R. V., Kislov A. M., Romanenko V. G., Fenchenko V. N. The software TRASSA for the analysis of spacecraft thermal conditions,  Kosm. nauka tehnol., 10 (4), 3—16 (2004) [in Russian].
2. Korn G.A., Korn Th.M. Mathematical handbook for scientists and engineers: definitions, theorems and formulas for reference and review, 720 p. (Nauka, Moscow, 1970) [in Russian].
3. Lizunov G. V., Glemba V. I., Korepanov V. E., et al. Space experiment "Potential" onboard the "Sich-2" satellite,  Kosm. nauka tehnol., 14 (4), 3—8 (2008) [in Russian].
https://doi.org/10.15407/knit2008.04.003