Works matching DE "ARTIFICIAL satellite re-entry"
Results: 19
Lessons learned in applying accelerometers to nuclear effects testing.
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- Shock & Vibration, 2008, v. 15, n. 6, p. 619, doi. 10.1155/2008/871916
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Application of the method for optimum filtering of measurements for determination and prediction of spacecraft orbits.
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- Solar System Research, 2013, v. 47, n. 7, p. 564, doi. 10.1134/S0038094613070113
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THE USE OF THE NASH BARGAINING MODEL IN TRAJECTORY SELECTION.
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- Management Science, 1976, v. 22, n. 7, p. 766, doi. 10.1287/mnsc.22.7.766
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Reentry Attitude Tracking Control for Hypersonic Vehicle with Reaction Control Systems via Improved Model Predictive Control Approach.
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- Computer Modeling in Engineering & Sciences (CMES), 2020, v. 122, n. 1, p. 131, doi. 10.32604/cmes.2020.08124
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Northern High-Latitude Precipitation as Depicted by Atmospheric Reanalyses and Satellite Retrievals.
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- Monthly Weather Review, 2005, v. 133, n. 12, p. 3407, doi. 10.1175/MWR3047.1
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Thermal-durability Evaluation of Inflatable Structure for a Deployable Aeroshell Using ICP Heater.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2018, v. 16, n. 6, p. 520, doi. 10.2322/tastj.16.520
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Constrained Adaptive Backstepping Control for Re-entry Vehicle.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 21
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Influence of Attack Angle on Magnetohydrodynamic Flow Control in Reentry Flight.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 13
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Control of Aerodynamic Characteristics of Lifting Reentry Vehicle with Applied Magnetic Field.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 7
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Empirical Study of the Lightweight Ablator Series for Transfer Vehicle Systems (LATS).
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 41
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Aerodynamic Simulation of Inflatable Re-Entry Vehicle Performance in Low Speed Wind Tunnel.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 57
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OPTIMAL TERMINAL DEFENSE TACTICS WHEN SEVERAL SEQUENTIAL ENGAGEMENTS ARE POSSIBLE.
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- Operations Research, 1987, v. 35, n. 4, p. 537, doi. 10.1287/opre.35.4.537
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Fluid/thermal/chemical non-equilibrium simulation of hypersonic reentry vehicles.
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- International Journal of Multiphysics, 2009, v. 3, n. 3, p. 293, doi. 10.1260/175095409788922284
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On the controllability of the roll rate of the ALFLEX reentry vehicle.
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- Nonlinear Studies, 2004, v. 11, n. 4, p. 543
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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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Flush air data sensing system.
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- Current Science (00113891), 2018, v. 114, n. 1, p. 68, doi. 10.18520/cs/v114/i01/68-73
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Drag reduction on a spiked body at hypersonic speed.
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- Aeronautical Journal, 2010, v. 114, n. 1152, p. 113
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Implementation of Surface Radiation and Fluid-Structure Thermal Coupling in Atmospheric Reentry.
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- International Journal of Aerospace Engineering, 2012, p. 1, doi. 10.1155/2012/402653
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Disturbance observer-based sliding mode backstepping control for a re-entry vehicle with input constraint and external disturbance.
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- Transactions of the Institute of Measurement & Control, 2016, v. 38, n. 2, p. 165, doi. 10.1177/0142331215572417
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- Article