Works matching DE "SPACE vehicle attitude control systems"
Results: 40
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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Electrodynamic control for spacecraft attitude stability in the geomagnetic field.
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- Cosmic Research, 2014, v. 52, n. 6, p. 472, doi. 10.1134/S001095251406001X
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Using extended Kalman filter and least squares method for spacecraft attitude estimation.
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- Mathematics in Engineering, Science & Aerospace (MESA), 2011, v. 2, n. 4, p. 445
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Modeling the angular motion dynamics of spacecraft with a magnetic attitude control system based on experimental studies and dynamic similarity.
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- Doklady Physics, 2017, v. 62, n. 12, p. 543, doi. 10.1134/S1028335817120011
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ANALYSIS OF MATRIX ALGORITHM OF ATTITUDE DETERMINATION.
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- Electronics & Control Systems, 2014, v. 4, n. 42, p. 45, doi. 10.18372/1990-5548.42.8810
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COMPARISON OF THE COVARIANCE ANALYSIS RESULTS OF THE QUEST AND THE TRIAD METHODS.
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- Electronics & Control Systems, 2014, v. 4, n. 42, p. 39, doi. 10.18372/1990-5548.42.8809
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A Bayesian Classifier for X-Ray Pulsars Recognition.
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- International Journal of Aerospace Engineering, 2016, p. 1, doi. 10.1155/2016/1746925
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Distributed attitude synchronization control for multiple flexible spacecraft without modal variable measurement.
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- International Journal of Robust & Nonlinear Control, 2018, v. 28, n. 10, p. 3435, doi. 10.1002/rnc.4092
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Robust adaptive fixed-time tracking control of 6-DOF spacecraft fly-around mission for noncooperative target.
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- International Journal of Robust & Nonlinear Control, 2018, v. 28, n. 6, p. 2598, doi. 10.1002/rnc.4038
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A simple saturated control framework for spacecraft with bounded disturbances.
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- International Journal of Robust & Nonlinear Control, 2016, v. 26, n. 3, p. 367, doi. 10.1002/rnc.3303
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Adaptive finite-time attitude stabilization for rigid spacecraft with actuator faults and saturation constraints.
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- International Journal of Robust & Nonlinear Control, 2016, v. 26, n. 1, p. 28, doi. 10.1002/rnc.3289
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Attitude tracking of rigid spacecraft subject to disturbances of unknown frequencies.
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- International Journal of Robust & Nonlinear Control, 2014, v. 24, n. 16, p. 2231, doi. 10.1002/rnc.2983
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Spacecraft chaotic attitude control with certain actuator failure based on integral sliding mode.
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- Journal of Engineering Research (2307-1877), 2018, v. 6, n. 1, p. 153
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Attitude stability of a dual-spin spacecraft on a stationary orbit around an asteroid subjected to gravity gradient torque.
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- Astrophysics & Space Science, 2015, v. 355, n. 2, p. 203, doi. 10.1007/s10509-014-2145-y
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Attitude stability of a spacecraft with two flexible solar arrays on a stationary orbit around an asteroid subjected to gravity gradient torque.
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- Astrophysics & Space Science, 2014, v. 351, n. 2, p. 507, doi. 10.1007/s10509-014-1863-5
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Anti-disturbance inverse optimal control for spacecraft position and attitude maneuvers with input saturation.
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- Advances in Mechanical Engineering (Sage Publications Inc.), 2016, v. 8, n. 5, p. 1, doi. 10.1177/1687814016649887
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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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Hybrid spacecraft attitude control system.
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- International Journal of Multiphysics, 2007, v. 1, n. 2, p. 221, doi. 10.1260/175095407781421586
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759. Feasibility and principle analyses of morphing airfoil used to control flight attitude.
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- Journal of Vibroengineering, 2012, v. 14, n. 1, p. 388
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Finite-Time Stabilization Control for a Rigid Spacecraft under Parameter Uncertainties.
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- Journal of Applied Mathematics, 2014, p. 1, doi. 10.1155/2014/816580
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Density interface topography recovered by inversion of satellite gravity gradiometry observations.
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- Journal of Geodesy, 2017, v. 91, n. 8, p. 881, doi. 10.1007/s00190-016-0993-7
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A Markley Variables-based Attitude Estimation Method Using Optical Flow and a Star Vector for Spinning Spacecraft.
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- Journal of Navigation, 2018, v. 71, n. 6, p. 1589, doi. 10.1017/S0373463318000516
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A Robust Optimization Approach for Magnetic Spacecraft Attitude Stabilization.
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- Journal of Optimization Theory & Applications, 2017, v. 173, n. 3, p. 994, doi. 10.1007/s10957-016-1035-6
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On the attitude stabilization of a rigid spacecraft using two skew control moment gyros.
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- Nonlinear Dynamics, 2015, v. 79, n. 3, p. 2079, doi. 10.1007/s11071-014-1796-0
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A robust attitude control strategy with guaranteed transient performance via modified Lyapunov-based control and integral sliding mode control.
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- Nonlinear Dynamics, 2014, v. 78, n. 3, p. 2205, doi. 10.1007/s11071-014-1598-4
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Optimal nonlinear feedback control of spacecraft rendezvous with finite low thrust between libration orbits.
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- Nonlinear Dynamics, 2014, v. 76, n. 2, p. 1611, doi. 10.1007/s11071-013-1233-9
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Finite-time output feedback attitude stabilisation for rigid spacecraft with input constraints.
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- IET Control Theory & Applications (Wiley-Blackwell), 2016, v. 10, n. 14, p. 1740, doi. 10.1049/iet-cta.2015.1174
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Star Image Prediction and Restoration under Dynamic Conditions.
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- Sensors (14248220), 2019, v. 19, n. 8, p. 1890, doi. 10.3390/s19081890
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Design and Simulation of a MEMS Control Moment Gyroscope for the Sub-Kilogram Spacecraft.
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- Sensors (14248220), 2010, v. 10, n. 4, p. 4130, doi. 10.3390/s100404130
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Spacecraft control with constrained fast reorientation and accurate pointing.
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- Aeronautical Journal, 2004, v. 108, n. 1080, p. 85, doi. 10.1017/S0001924000005030
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Constrained large angle reorientation manoeuvres of a space telescope using potential functions and a variable control gain.
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- Aeronautical Journal, 2013, v. 117, n. 1194, p. 807, doi. 10.1017/S0001924000008460
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Optimal Attitude Control for Spacecraft Using Two Variable-Speed Control Moment Gyros.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 3, p. 371, doi. 10.2322/tastj.17.371
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On Port-Hamiltonian Modeling and Control of Systems with Quaternions.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 1
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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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Achievement of Long-term On-orbit Operation of the SIMPLE Inflatable Extension Mast.
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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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Spacecraft Attitude Control with RWs via LPV Control Theory: Comparison of Two Different Methods in One Framework.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 15
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Spacecraft Attitude Control Using a Control Moment Gyro with Multiple Degrees of Freedom.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 75
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Design and Implementation of a Thermopile-Based Earth Sensor.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 77
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New Chattering Attenuation Sliding Mode Control of a Flexible Spacecraft.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 71
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Sensor fault accommodation for the attitude control system of near space vehicle based on T-S fuzzy modeling approach.
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- Journal of Hebei University of Science & Technology, 2013, v. 34, n. 6, p. 552, doi. 10.7535/hbkd.2013yx06011
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