On the Possibility of Increasing Rocky Target Penetration Depth for Compound Penetrators Featuring a Tail Assembly Jettisoned at Impact
Authors: Fedorov S.V., Veldanov V.A., Fedorova N.A. | Published: 17.02.2019 |
Published in issue: #1(124)/2019 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
Keywords: high-speed penetration, rocky ground target, penetrator, penetrating unit, ballast mass jettisoning, recoil impulse |
Development of a Launch Vehicle Control Algorithm at the Initial Flight Part in Case of one of the Engines
Authors: Trifonov M.V., Altshuler A.Sh., Bobronnikov V.T. | Published: 17.02.2019 |
Published in issue: #1(124)/2019 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
Keywords: launch vehicle, launch complex safety, engine failure, emergency displacement, optimal regulator, quadratic criterion |
Estimating Feasibility of Taking Quadratic Terms into Account During Guidance Error Analysis for the Case of Interplanetary Spacecraft
Authors: Sukhova S.V. | Published: 10.04.2018 |
Published in issue: #2(119)/2018 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
Keywords: guidance error analysis, Monte Carlo method, interplanetary transfer |
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 |
To the calculation of the main vector and the main momentum of light pressure force on a solar sail
Authors: Zimin V.N. , Nerovnyi N.A. | Published: 14.02.2016 |
Published in issue: #1(106)/2016 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
Keywords: solar sail, light pressure, reflectivity coefficient, optical characteristics, resultant vector, principal moment |
Dynamics of manned spaceship fairing elements motion in emergency
Authors: Kokushkin V.V., Khomyakov M.K., Ovsyannikova N.Yu. | Published: 14.02.2016 |
Published in issue: #1(106)/2016 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
Keywords: spaceship, reentry module, separated nose fairing, emergency abort, separation dynamics, interaction force |
Ballistic and navigation issues for satellite formation flying design
Authors: Palkin M.V. | Published: 21.12.2015 |
Published in issue: #6(105)/2015 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
Keywords: spacecraft formation flying, leader satellite, slave satellite, satellite navigation system, single-level control structure, multilevel control structure |
Spacecraft optimal control in drag braking flight segment during insertion into orbit of Mars artificial satellite
Authors: Sokolov N.L. | Published: 21.12.2015 |
Published in issue: #6(105)/2015 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
Keywords: spacecraft, insertion into orbit, combined insertion profile, optimal control, research technique, analytical algorithm, implementation efficiency |
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 |