Abstract
A change in the angle of attack oscillation amplitude in the spatial motion of an uncontrolled landing module at the restoring moment, described by the odd Fourier series with respect to the angle of attack with the first three harmonics, is considered. Phase trajectory evolution is studied based on an analysis of the action integral, for which the analytical expressions have been found. The formula for the time of appearance of additional equilibrium positions on the phase portrait and for the time of transition between different phase plane regions has been found. The formulas for determining the probability of capture in any region have been found for situations of motion when a phase point can fall in different oscillation regions when crossing the separatrix.
Similar content being viewed by others
References
Kuzmak, G.E., Dinamika neupravlyaemogo dvizheniya letatel’nykh apparatov pri vkhode v atmosferu (Dynamics of Uncontrollable Motion of Spacecraft at Reentry into the Atmosphere), Moscow: Nauka, 1970.
Yaroshevskii, V.A., Dvizhenie neupravlyaemogo tela v atmosfere (Motion of an Uncontrollable Body in the Atmosphere), Moscow: Mashinostroenie, 1978.
Yaroshevskii, V.A., Analytical estimates of peak amplitudes of oscillations of the angle of attack for uncontrolled spacecraft entering into the atmosphere: A case of plane motion, Kosm. Issled., 2000, vol. 38, no. 4, pp. 437–442. [Cosmic Research, pp. 410–414].
Aslanov, V.S. and Timbai, I.A., Transient modes of spacecraft angular motion on the upper section of the reentry trajectory, Kosm.. Issled., 1997, vol. 35, no. 3, pp. 279–286. [Cosmic Research, pp. 260–267].
Kenshov, E.A. and Timbai, I.A., Transition of planar rotational motion of an asymmetric spacecraft into oscillatory motion at its reentry into the atmosphere., Kosm. Issled., 2004, vol. 42, no. 3, pp. 295–301. [Cosmic Research, pp. 283–288].
Aslanov, V.S. and Ledkov, A.S., Features of rotational motion of a spacecraft descending in the Martian atmosphere, Kosm. Issled., 2007, vol. 45, no., pp. 351–357. [Cosmic Research, pp. 331–338].
Barinova E.V. and Timbai I.A., Investigation of planar attitude motion of a descent module with triharmonic moment characteristics at reentry into the atmosphere, Kosm. Issled., 2014, vol. 52, no. 4, p. 337.
Neishtadt, A.I., On variation of the adiabatic invariant when crossing a separatrix, Fizika Plazmy, 1986, vol.12, no. 8, pp. 992–1001.
Lifshits, I.M., Slutskin, A.A, and Nabutovskii, V.M., Peculiarities of charged particle motion in a variable and inhomogeneous electromagnetic field, Zhurn. Eksp. Teor.. Fiz., 1961, vol. 41, no. 3, pp. 939–948.
Aslanov, V.S., Prostranstvennoe dvizhenie tela pri spuske v atmosfere (Three-dimensional Motion of a Body during Its Descent in the Atmosphere), Moscow: Fizmatlit, 2004.
Author information
Authors and Affiliations
Corresponding author
Additional information
Original Russian Text © E.V. Barinova, I.A. Timbai, 2015, published in Kosmicheskie Issledovaniya, 2015, Vol. 53, No. 3, pp. 263–272.
Rights and permissions
About this article
Cite this article
Barinova, E.V., Timbai, I.A. Studying transient motion modes with respect to the landing module angle of attack with the restoring moment triharmonic characteristic on entering the atmosphere. Cosmic Res 53, 246–255 (2015). https://doi.org/10.1134/S001095251502001X
Received:
Published:
Issue Date:
DOI: https://doi.org/10.1134/S001095251502001X