MainCatalogAviation, Rocket and Space EngineeringDynamics, Ballistics, Flying Vehicle Motion Control
Synthesizing Relay-Based Spacecraft Attitude Control and Stabilization Ensuring High Quality without Velocity Sensors
| Authors: Simonyants R.P., Averyanov P.V. | Published: 13.06.2018 |
| Published in issue: #3(120)/2018 | |
| DOI: 10.18698/0236-3933-2018-3-104-119 | |
| Category: Aviation, Rocket and Space Engineering | Chapter: Dynamics, Ballistics, Flying Vehicle Motion Control | |
| Keywords: relay-based stabilisation, internal feedback, velocity sensor, attitude control, alignment diagram method, sliding mode | |
Method of Increasing the Monitoring Frequency of the Inspecting Area by Earth Remote Sensing Spacecraft
| Authors: Salov V.V., Protsenko P.A., Khubbiev R.V. | Published: 09.02.2018 |
| Published in issue: #1(118)/2018 | |
| DOI: 10.18698/0236-3933-2018-1-105-114 | |
| Category: Aviation, Rocket and Space Engineering | Chapter: Dynamics, Ballistics, Flying Vehicle Motion Control | |
| Keywords: earth remote sensing spacecraft, iso-path orbit, monitoring, area | |
On the Solution to the Problem of Guiding an Illumination-Providing Satellite Towards the Specified Earth‘s Surface Region, and Estimation of Illumination Intensity
| Authors: Sumarokov A.V., Timakov S.N., Bogdanov K.A. | Published: 29.11.2017 |
| Published in issue: #6(117)/2017 | |
| DOI: 10.18698/0236-3933-2017-6-115-129 | |
| Category: Aviation, Rocket and Space Engineering | Chapter: Dynamics, Ballistics, Flying Vehicle Motion Control | |
| Keywords: solar sail spacecraft, illumination providing satellite, space tests, guidance | |
Algorithm of ISS Optimal Propellant Maneuver with Path Constraints in ISS Structure Loads
| Authors: Atroshenkov S.N., Platonov V.N., Gubarev F.V., Saratov A.A. | Published: 02.08.2017 |
| Published in issue: #4(115)/2017 | |
| DOI: 10.18698/0236-3933-2017-4-118-138 | |
| Category: Aviation, Rocket and Space Engineering | Chapter: Dynamics, Ballistics, Flying Vehicle Motion Control | |
| Keywords: elastic oscillations of ISS structure, critical interfaces, limit loads, ISS thrusters, Optimal Propellant Maneuver (ОРМ), optimization algorithms | |
UAV Adaptive Automatic Control at Rendezvous and Docking Stage in Inflight Refueling
| Authors: Voronov E.M., Obolensky Yu.G., Cheglakov D.I. | Published: 28.05.2017 |
| Published in issue: #3(114)/2017 | |
| DOI: 10.18698/0236-3933-2017-3-129-147 | |
| Category: Aviation, Rocket and Space Engineering | Chapter: Dynamics, Ballistics, Flying Vehicle Motion Control | |
| Keywords: inflight reveling, probe, cone, adaptive control, state observer | |
Method for Identification of Second-Order Link Parameters with Classical Dry (Coulomb) Friction for Analysis and Synthesis of Nonlinear Dynamic Objects and Control Systems
| Authors: Belonogov O.B. | Published: 28.05.2017 |
| Published in issue: #3(114)/2017 | |
| DOI: 10.18698/0236-3933-2017-3-118-128 | |
| Category: Aviation, Rocket and Space Engineering | Chapter: Dynamics, Ballistics, Flying Vehicle Motion Control | |
| Keywords: frequency response characteristics, nonlinear dynamic objects, control systems, frequency identification | |
On the Loads on Multipurpose Laboratory Module Construction Elements During the Autonomous Flight Phase
| Authors: Prut’ko A.A., Sumarokov A.V. | Published: 12.04.2017 |
| Published in issue: #2(113)/2017 | |
| DOI: 10.18698/0236-3933-2017-2-123-138 | |
| Category: Aviation, Rocket and Space Engineering | Chapter: Dynamics, Ballistics, Flying Vehicle Motion Control | |
| Keywords: International Space Station, multipurpose laboratory module, Russian segment, eigenfrequencies, loads on construction, guidance, navigation and control system | |
Increased accuracy in determining the orbital parameters based on convolution operators application as a result of small interval GLONASS data processing
| Authors: Antsev G.V., Lysenko L.N., Petrov V.A. | Published: 12.10.2016 |
| Published in issue: #5(110)/2016 | |
| DOI: 10.18698/0236-3933-2016-5-99-110 | |
| Category: Aviation, Rocket and Space Engineering | Chapter: Dynamics, Ballistics, Flying Vehicle Motion Control | |
| Keywords: orbital parameters, filter monitoring interval, convolution assessment, combination of assessments, reduction factor dispersions | |
Algorithm of Thruster Failure Detection for the International Space Station Based on Self-Adjusting Onboard Model of Angular Motion Dynamics
| Authors: Zhirnov A.V., Timakov S.N. | Published: 12.08.2016 |
| Published in issue: #4(109)/2016 | |
| DOI: 10.18698/0236-3933-2016-4-98-114 | |
| Category: Aviation, Rocket and Space Engineering | Chapter: Dynamics, Ballistics, Flying Vehicle Motion Control | |
| Keywords: failure detection, thruster failure, self-adjust onboard model, adaptive observer, elastic vibrations of structure | |
On Pointing of High Resolution Camera Mounted on the International Space Station using Biaxial Rotating Platform
| Authors: Sumarokov A.V. | Published: 12.08.2016 |
| Published in issue: #4(109)/2016 | |
| DOI: 10.18698/0236-3933-2016-4-85-97 | |
| Category: Aviation, Rocket and Space Engineering | Chapter: Dynamics, Ballistics, Flying Vehicle Motion Control | |
| Keywords: the International space station, space experiments, Napor-Mini RSA, pointing, the Earth remote sensing, biaxial pointing platform | |