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