Transition of Planar Rotational Motion of an Asymmetric Spacecraft into Oscillatory Motion at Its Reentry into the Atmosphere

By Kenshov E. A.   Timbai I. A.  

Cosmic Research, Vol. 42, Iss. 3, 2004-05 ,pp. : 283-288

MAIK Nauka/Interperiodica

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Robust algorithm of control for a maneuver in the Martian atmosphere to insert a spacecraft into the planet’s satellite orbit

By Sikharulidze Yu.   Korchagin A.   Zhukov B.  

Cosmic Research, Vol. 45, Iss. 4, 2007-08 ,pp. : 317-330

MAIK Nauka/Interperiodica

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Determination of the width of a corridor of re-entry into the atmosphere for the problem of launching a spacecraft into a circumplanetary orbit after braking in the atmosphere

By Yaroshevskii V.  

Cosmic Research, Vol. 44, Iss. 3, 2006-05 ,pp. : 236-244

MAIK Nauka/Interperiodica

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Motion of a Load along a Cable Fastened to a Two-Body-Tethered Spacecraft

By Rodnikov A. V.  

Cosmic Research, Vol. 42, Iss. 4, 2004-07 ,pp. : 427-431

MAIK Nauka/Interperiodica

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Attitude motion of spacecraft during oblique solar panel deployment

By Zhengfeng Bai   Yang Zhao  

Aircraft Engineering, Vol. 84, Iss. 2, 2012-03 ,pp. : 109-114

Emerald Group Publishing Ltd

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