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|
|Section: Spacecraft Dynamics and Control|
|Publication Language: Russian|
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|
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