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All articles by "Kazakovtsev V.P. "

Correction of spacecraft trajectory during its transition into circular satellite orbit using atmospheric braking with uncertain atmospheric parameters

Authors: Kazakovtsev V.P. , Koryanov V.V. , Zaw Min Tun Published: 06.10.2015
Published in issue: #5(104)/2015  
DOI:

DOI: 10.18698/0236-3941-2015-5-38-46

  
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control  
Keywords: orbit, spatial motion, spacecraft, braking in atmosphere, heat flow, dynamic pressure

Simulation of dynamic motion in Earth atmosphere for lander intended to be descented in Mars atmosphere

Authors: Kazakovtsev V.P.  Published: 24.05.2015
Published in issue: #3(32)/1998  
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Category: Simulation of Processes  
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Motion Dynamics Study of Descent Module with Non-Stiff Construction Elements

Authors: Kazakovtsev V.P. , Mitchenkova A.A. Published: 16.11.2014
Published in issue: #4(49)/2002  
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Category: Simulation of Processes  
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Method for calculating spacecraft longitudinal motion parameters during landing on the surface of a small celestial body

Authors: Kazakovtsev V.P. , Chen Danhe, Koryanov V.V.  Published: 06.02.2014
Published in issue: #1(94)/2014  
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Category: Simulation of Processes  
Keywords: landing on small celestial bodies, method for dynamics analysis of spacecraft motion, evaluation of influence of disturbing factors, conditions for safe landing

On Using Preliminary Braking Impulse in Spacecraft Injection into Orbit of Mars Satellite

Authors: Kazakovtsev V.P. , Sukhenko A.V. Published: 31.01.2014
Published in issue: #4(61)/2005  
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Category: Simulation of Processes  
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Method for Studying Dynamics of Angular Motion of Descent Spacecraft with Inflatable Brake Device

Authors: Kazakovtsev V.P. , Koryanov V.V.  Published: 11.09.2013
Published in issue: #3(88)/2012  
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Category: Simulation of Processes  
Keywords: descent spacecraft, dynamics, inflatable brake device, atmospheric descent, simulation, asymmetry
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