Method for Estimating the Efficiency of Small Orbital Spacecraft Systems for Optoelectronic Surveillance
| Authors: Protsenko P.A., Khubbiev R.V. | Published: 16.02.2020 |
| Published in issue: #1(130)/2020 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: efficiency, object sighting time delay, optoelectronic surveillance, orbital system, small spacecraft | |
Group-Theoretical Analysis of the Clustered Launch Vehicle Dynamics
| Authors: Pavlov A.M. | Published: 03.09.2019 |
| Published in issue: #4(127)/2019 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: launch vehicle, beam system, symmetry group, vibration frequency, irreducible representation, orthoprojector | |
Accounting for Nonlinear Ship Motion in Navigational al Support of Submarine Ballistic Missile Launches
| Authors: Antsev G.V., Lysenko L.N., Petrov V.A. | Published: 22.04.2019 |
| Published in issue: #2(125)/2019 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: nonlinear ship motion models, optimum filtering, ballistic missile, submarine, inertial navigation system, pre-launch sequence, using velocity to determine initial conditions | |
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 | |