Studying transient motion modes with respect to the landing module angle of attack with the restoring moment triharmonic characteristic on entering the atmosphere

Author:

Barinova E. V.,Timbai I. A.

Publisher

Pleiades Publishing Ltd

Subject

Space and Planetary Science,Astronomy and Astrophysics,Aerospace Engineering

Reference10 articles.

1. 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.

2. Yaroshevskii, V.A., Dvizhenie neupravlyaemogo tela v atmosfere (Motion of an Uncontrollable Body in the Atmosphere), Moscow: Mashinostroenie, 1978.

3. 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].

4. 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].

5. 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].

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