Works matching DE "SPACE vehicle control systems"
Results: 86
Multi⁃spacecraft Intelligent Orbit Phasing Control Considering Collision Avoidance.
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- Transactions of Nanjing University of Aeronautics & Astronautics, 2022, v. 39, n. 4, p. 379, doi. 10.16356/j.1005-1120.2022.04.001
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Robust Adaptive Attitude Maneuvering and Vibration Reducing Control of Flexible Spacecraft with Prescribed Performance.
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- Transactions of Nanjing University of Aeronautics & Astronautics, 2019, v. 36, n. 2, p. 214, doi. 10.16356/j.1005-1120.2019.02.004
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Attitude Determination and Control System for the PROCYON Micro-Spacecraft.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2017, v. 60, n. 3, p. 181, doi. 10.2322/tjsass.60.181
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Computation of program controls performed nonstop by gyrodynes.
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- Doklady Mathematics, 2017, v. 96, n. 2, p. 528, doi. 10.1134/S1064562417050027
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Construction of optimum controls and trajectories of motion of the center of masses of a spacecraft equipped with the solar sail and low-thrust engine, using quaternions and Kustaanheimo-Stiefel variables.
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- Cosmic Research, 2014, v. 52, n. 6, p. 450, doi. 10.1134/S0010952514060057
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Features of RadioAstron Mission Control.
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- Cosmic Research, 2014, v. 52, n. 5, p. 326, doi. 10.1134/S0010952514050062
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Effect of thin condensate films of a metal working fluid of an electric propulsion engine on the integral optical coefficients of a spacecraft's thermal control coating.
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- Cosmic Research, 2014, v. 52, n. 3, p. 235, doi. 10.1134/S0010952514030034
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Controlling spacecraft by means of solar radiation.
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- Cosmic Research, 2014, v. 52, n. 3, p. 244, doi. 10.1134/S0010952514030046
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The Rate of Single Event Upsets in Electronic Circuits onboard Spacecraft.
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- Cosmic Research, 2005, v. 43, n. 6, p. 423, doi. 10.1007/s10604-005-0066-9
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Approximate Calculation of Required and Available Lateral Range Achieved in a Spacecraft Descent to a Preset Point on the Earth's Surface.
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- Cosmic Research, 2005, v. 43, n. 6, p. 442, doi. 10.1007/s10604-005-0068-7
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An Effective Algorithm of Aerodynamic Control over Spacecraft Descent.
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- Cosmic Research, 2005, v. 43, n. 6, p. 450, doi. 10.1007/s10604-005-0069-6
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Filled Aluminosilicate of Dendrimer Morphology Used as Low Temperature Cofired Ceramic in LED Devices and Spacecraft Control Systems.
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- Journal of Nano- & Electronic Physics, 2015, v. 7, n. 4, p. 04031-1
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Nonlinear dynamics of mini-satellite respinup by weak internal control torques.
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- Mathematics in Engineering, Science & Aerospace (MESA), 2015, v. 6, n. 1, p. 11
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Spacecraft combined attitude and sun tracking (CAST) system.
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- Mathematics in Engineering, Science & Aerospace (MESA), 2011, v. 2, n. 4, p. 413
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AROUND THE CIRCUIT.
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- Microwave Journal, 2004, v. 47, n. 3, p. 54
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Analysis of Efficiency of Systems for Control of the Thermal Regime of Spacecraft.
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- Chemical & Petroleum Engineering, 2016, v. 51, n. 9/10, p. 714, doi. 10.1007/s10556-016-0110-z
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GRB Satellites.
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- Mercury, 2010, v. 39, n. 2, p. 30
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The necessity of introducing a geometric control subsystem into the composite attitude control systems of spacecraft and aircraft with modern precision.
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- Doklady Physics, 2016, v. 61, n. 1, p. 5, doi. 10.1134/S1028335816010079
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Formal Analysis of a Space-Craft Controller Using SPIN.
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- IEEE Transactions on Software Engineering, 2001, v. 27, n. 8, p. 749, doi. 10.1109/32.940728
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Attitude and Vibration Control of Flexible Spacecraft Using Singular Perturbation Approach.
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- ISRN Otolaryngology, 2014, p. 1, doi. 10.1155/2014/163870
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Control theoretic analysis of a target search problem by a team of search vehicles.
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- International Journal of Control, 2008, v. 81, n. 12, p. 1878, doi. 10.1080/00207170801927155
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What is a limit cycle?
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- International Journal of Control, 2008, v. 81, n. 12, p. 1886, doi. 10.1080/00207170801927163
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Spin-axis stabilisation of underactuated rigid spacecraft under sinusoidal disturbance.
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- International Journal of Control, 2008, v. 81, n. 12, p. 1901, doi. 10.1080/00207170801930217
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ANALYSIS OF THE EFFECT OF SOFT SOIL'S PARAMETERS CHANGE ON PLANETARY VEHICLES' DYNAMIC RESPONSE.
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- Journal of Automation, Mobile Robotics & Intelligent Systems, 2017, v. 11, n. 4, p. 65, doi. 10.14313/JAMRIS_4-2017/37
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Concise Neural Nonaffine Control of Air-Breathing Hypersonic Vehicles Subject to Parametric Uncertainties.
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- International Journal of Aerospace Engineering, 2017, p. 1, doi. 10.1155/2017/1374932
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Autonomous Rendezvous and Docking with Nonfull Field of View for Tethered Space Robot.
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- International Journal of Aerospace Engineering, 2017, p. 1, doi. 10.1155/2017/3162349
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Formation Flight Control.
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- International Journal of Aerospace Engineering, 2011, p. 1, doi. 10.1155/2011/798981
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Guidance Navigation and Control for AutonomousMultiple Spacecraft Assembly: Analysis and Experimentation.
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- International Journal of Aerospace Engineering, 2011, p. 1, doi. 10.1155/2011/308245
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Cascade-Based Controlled Attitude Synchronization and Tracking of Spacecraft in Leader-Follower Formation.
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- International Journal of Aerospace Engineering, 2011, p. 1, doi. 10.1155/2011/151262
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UAVs Dynamic Mission Management in Adversarial Environments.
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- International Journal of Aerospace Engineering, 2009, p. 1, doi. 10.1155/2009/107214
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Reaction wheel fault tolerant control for spacecraft attitude stabilization with finite-time convergence.
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- International Journal of Robust & Nonlinear Control, 2013, v. 23, n. 15, p. 1737, doi. 10.1002/rnc.2924
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Методические основы проектирования стационарных систем термостатирования ракет космического назначения на низко- и высококипящих компонентах топлива
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- Refrigeration Engineering & Technology, 2017, v. 53, n. 6, p. 39
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CONTROL DEPLOYMENT OF MOBILE UNITS OF LARGE-SIZED SPACECRAFT.
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- Annals of DAAAM & Proceedings, 2017, v. 28, p. 773, doi. 10.2507/28th.daaam.proceedings.109
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Calibration of Airdata Systems Using Extended Kalman Filtering Technique.
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- International Journal of Aerospace Innovations, 2010, v. 2, n. 1/2, p. 133
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Fault Tolerant Control for Near Space Vehicles with Input Saturation Using Disturbance Observer and Neural Networks.
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- Circuits, Systems & Signal Processing, 2015, v. 34, n. 7, p. 2091, doi. 10.1007/s00034-014-9939-6
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Analysis of Reduction of Controllability of Spacecraft During Conducting of Active Control Over Microaccelerations.
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- International Review of Aerospace Engineering, 2017, v. 10, n. 3, p. 160, doi. 10.15866/irease.v10i3.12342
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Investigation and Optimization of Disk-Laser Welding of 1 mm Thick Ti-6Al-4V Titanium Alloy Sheets.
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- Advances in Mechanical Engineering (Sage Publications Inc.), 2015, v. 7, n. 1, p. 1, doi. 10.1155/2014/373561
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Robust Adaptive Learning Control for Spacecraft Autonomous Proximity Maneuver.
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- International Journal of Pattern Recognition & Artificial Intelligence, 2017, v. 31, n. 5, p. -1, doi. 10.1142/S0218001417590078
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Mathematical modeling of spacecraft guidance and control system in 3D space orbit transfer mission.
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- Computational & Applied Mathematics, 2016, v. 35, n. 3, p. 865, doi. 10.1007/s40314-015-0290-8
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Flexspline Deformation Analysis Depending on the Polymer Material Used in the Harmonic Drive Prototype.
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- Technical Gazette / Tehnički Vjesnik, 2024, v. 31, n. 6, p. 2087, doi. 10.17559/TV-20230203000316
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Shorter Path Design and Control for an Underactuated Satellite.
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- International Journal of Aerospace Engineering, 2017, p. 1, doi. 10.1155/2017/8536732
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In-orbit attitude actuation using solar panels.
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- International Journal of Multiphysics, 2008, v. 2, n. 2, p. 147, doi. 10.1260/175095408785416956
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GAUGE: the GrAnd Unification and Gravity Explorer.
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- Experimental Astronomy, 2009, v. 23, n. 2, p. 549, doi. 10.1007/s10686-008-9086-9
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An optimal control approach to spacecraft rendezvous on elliptical orbit.
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- Optimal Control - Applications & Methods, 2015, v. 36, n. 2, p. 158, doi. 10.1002/oca.2108
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Active Spacecraft Potential Control Investigation.
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- Space Science Reviews, 2016, v. 199, n. 1-4, p. 515, doi. 10.1007/s11214-014-0049-3
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Modal filter as a device for electrostatic discharge protection of onboard computers and control units of space vehicles.
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- Russian Physics Journal, 2012, v. 55, n. 3, p. 282, doi. 10.1007/s11182-012-9808-3
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Human Performance Time Model of Spacecraft Control Panel Operation in Simulated Microgravity.
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- Aerospace Medicine & Human Performance, 2017, v. 88, n. 8, p. 743, doi. 10.3357/AMHP.4668.2017
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Multiple-Subarc Gradient-Restoration Algorithm, Part 2: Application to a Multistage Launch Vehicle Design.
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- Journal of Optimization Theory & Applications, 2003, v. 116, n. 1, p. 19, doi. 10.1023/A:1022154001343
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The OSIRIS instrument on the Odin spacecraft.
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- Canadian Journal of Physics, 2004, v. 82, n. 6, p. 411, doi. 10.1139/P04-005
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Robust Adaptive Control of a Large Spacecraft.
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- Engineering Letters, 2008, v. 16, n. 3, p. 321
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