Abstract
This paper is about research of dynamics of spatial motion of two-blade heliogyro solar sail considering different types of perturbing effects with their responsiveness and range. The main purpose of this work is determination of list of design objectives and their range to provide sustainable movement of picosatellite with two-blade solar sail in experiment BMSTU-Sail.
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Mayorova, V. I., Dmitriev A., Nerovnyy N., Rachkin D., Tenenbaum S., “ISS - test bed for the future solar sail systems”, 63 rd International Astronautical Congress, IAC-12-B3.3.10, Naples, Italy, 2012.
Weisstein, Eric W. “Monte Carlo Method.” From MathWorld-A Wolfram Web Resource. http://mathworld.wolfram.com/MonteCarloMethod.html [cited 10 May 2013].
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Mayorova, V., Popov, A., Nerovnyy, N., Rachkin, D., Tenenbaum, S. (2014). Two-Blade Solar Sail Dynamics. In: Macdonald, M. (eds) Advances in Solar Sailing. Springer Praxis Books(). Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-34907-2_44
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DOI: https://doi.org/10.1007/978-3-642-34907-2_44
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