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All articles by "Koryanov V.V. "

Expanding Possible Landing Areas on the Surface of Venus by using Gravity Assist Maneuvers

Authors: Nazirov R.R., Eismont N.A., Zubko V.A., Belyaev A.A., Fedyaev K.S., Zasova L.V., Gorinov D.A., Simonov A.V., Koryanov V.V.  Published: 27.06.2022
Published in issue: #2(141)/2022  
DOI:

DOI: 10.18698/0236-3941-2022-2-20-42

  
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control  
Keywords: automatic interplanetary station "Venera-D", lander, landing area, gravity assistmaneuver, resonant orbit, Venus

Multiple Regression for UAV Aerodynamic Model based on Experimental Data

Authors: Koryanov V.V. , Nguyen K.T., Nguyen V.T. Published: 19.10.2016
Published in issue: #5(110)/2016  
DOI:

DOI: 10.18698/0236-3941-2016-5-59-67

  
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control  
Keywords: multiple regression, statistical synthesis, aerodynamic model, structural and parametric selection criterion, Unmanned Aerial Vehicle (UAV), correlation

Evaluation of satellite navigation accuracy requirements based on the analysis of the current state of commercial coordinate and time navigation support systems

Authors: Lysenko L.N., Koryanov V.V. , Toporkov A.G. Published: 06.10.2015
Published in issue: #5(104)/2015  
DOI:

DOI: 10.18698/0236-3941-2015-5-47-61

  
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control  
Keywords: global navigation satellite system, commercial systems, ballistic and navigational support, accuracy

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

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  
DOI:

DOI:

 
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

Technique to Compute Parameters of Dynamics of Descent Vehicle Movement with Hard Landing onto Planet Surface

Authors: Koryanov V.V.  Published: 03.02.2014
Published in issue: #1(74)/2009  
DOI:

DOI:

 
Category: Simulation of Processes  
Keywords:

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  
DOI:

DOI:

 
Category: Simulation of Processes  
Keywords: descent spacecraft, dynamics, inflatable brake device, atmospheric descent, simulation, asymmetry
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