Works matching DE "ARTIFICIAL satellite attitude control systems"
Results: 893
Geometry-Based Doppler Analysis for GPS Receivers.
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- Wireless Personal Communications, 2013, v. 68, n. 1, p. 1, doi. 10.1007/s11277-011-0435-z
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基于新型趋近律的四旋翼滑模控制.
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- Electronic Science & Technology, 2024, v. 37, n. 12, p. 1, doi. 10.16180/j.cnki.issn1007-7820.2024.12.001
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基于反步法的四旋翼无人机自适应控制研究.
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- Electronic Science & Technology, 2022, v. 35, n. 3, p. 32, doi. 10.16180/j.cnki.issn1007-7820.2022.03.005
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针叶林冠层热点及多角度无人机遥感观测及 特征分析.
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- Journal of Remote Sensing, 2021, v. 25, n. 4, p. 1013, doi. 10.11834/jrs.20219435
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CX-6(02)微纳卫星超分辨率成像.
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- Journal of Remote Sensing, 2019, v. 23, n. 2, p. 196, doi. 10.11834/jrs.20198014
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Abstracts of the Papers Published in Journal of the Japan Society for Aeronautical and Space Sciences (Vol. 72, No. 6, Dec. 2024).
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- Transactions of the Japan Society of Aeronautical & Space Science, 2025, v. 68, n. 1, p. 68, doi. 10.2322/tjsass.68.68
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Abstracts of the Papers Published in Journal of the Japan Society for Aeronautical and Space Sciences (Vol. 71, No. 6, Dec. 2023).
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- Transactions of the Japan Society of Aeronautical & Space Science, 2024, v. 67, n. 1, p. 40, doi. 10.2322/tjsass.67.40
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Experimental Verification for Attitude Control of Spacecraft Utilizing Double-Gimbal Variable-Speed Control Moment Gyroscopes.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2023, v. 66, n. 6, p. 209, doi. 10.2322/tjsass.66.209
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Multi-objective Optimization of Observation Scheduling Avoiding Attitude Maneuvering Conflict.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2022, v. 65, n. 2, p. 66, doi. 10.2322/tjsass.65.66
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Performance Evaluation of Combustion-controllable 0.1-N-Class Solid Propellant Microthrusters Using Laser Heating.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2021, v. 64, n. 2, p. 65, doi. 10.2322/tjsass.64.65
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Attitude Determination Algorithm Using Earth Sensor Images and Image Recognition.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2021, v. 64, n. 2, p. 82, doi. 10.2322/tjsass.64.82
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Dual Manipulator-Actuated Integrated Translational and Rotational Stabilization of Spacecraft in Proximity Operations.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2020, v. 63, n. 5, p. 195, doi. 10.2322/tjsass.63.195
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Development of a Novel Core Component-based Flight Dynamics Subsystem Software Platform.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2019, v. 62, n. 4, p. 192, doi. 10.2322/tjsass.62.192
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Fast Slew Maneuvers for the High-Torque-Wheels BIROS Satellite.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2018, v. 61, n. 2, p. 79, doi. 10.2322/tjsass.61.79
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Practical Solution to Efficient Flight Path Control for Hypersonic Vehicles.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2016, v. 59, n. 4, p. 195, doi. 10.2322/tjsass.59.195
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面向用户随机分布的NOMA-卫星通信网络性能分析.
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- Telecommunication Engineering, 2020, v. 60, n. 2, p. 153, doi. 10.3969/j issn.1001-893x.2020.02.005
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Mapping Nature-based Marine Flooding Risk using VHR Wave, Airborne LiDAR and Satellite Imagery: The Case Study of the Dol Marsh (Bay of Mont-Saint-Michel, France).
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- Journal of Coastal Research, 2020, v. 95, p. 743, doi. 10.2112/SI95-145.1
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Satellite Attitude Control System Design considering the Fuel Slosh Dynamics.
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- Shock & Vibration, 2014, p. 1, doi. 10.1155/2014/260206
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Application of the state-dependent riccati equation and kalman filter techniques to the design of a satellite control system.
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- Shock & Vibration, 2012, v. 19, n. 5, p. 939, doi. 10.1155/2012/716975
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Design of a nonlinear controller for a rigid-flexible satellite using multi-objective Generalized Extremal Optimization with real codification.
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- Shock & Vibration, 2012, v. 19, n. 5, p. 947, doi. 10.1155/2012/254895
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Satellite attitude control system simulator.
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- Shock & Vibration, 2008, v. 15, n. 3/4, p. 395, doi. 10.1155/2008/141465
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Satellite attitude control system simulator.
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- Shock & Vibration, 2008, p. 395, doi. 10.1155/2008/141465
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考虑瞬态特性的无人机自适应容错控制设计 .
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- Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2023, v. 55, n. 1, p. 89, doi. 10.16356/j.1005‑2615.2023.01.011
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变质心共轴双旋翼无人机建模与反步滑模控制.
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- Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2022, v. 54, n. 6, p. 1056, doi. 10.16356/j.1005⁃2615.2022.06.007
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基于无迹卡尔曼滤波的柔性自由翻滚目标姿态估计.
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- Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2022, v. 54, n. 1, p. 51, doi. 10.16356/j.1005-2615.2022.01.006
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无人机绕速度矢量轴滚转机动自适应 滑模边界保护控制.
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- Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2021, v. 53, n. 6, p. 918, doi. 10.16356/j.1005-2615.2021.06.011
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基于未知输入观测器的四旋翼无人机故障诊断与模型 参考容错控制.
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- Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2020, v. 52, n. 6, p. 889, doi. 10.16356/j.1005⁃2615.2020.06.007
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Identification Technology of Modal Parameter of a Strap-on Launch Vehicle.
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- International Journal of Computational Methods, 2016, v. 13, n. 1, p. -1, doi. 10.1142/S0219876216500109
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Conflict without an Apparent Cause.
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- Games (20734336), 2019, v. 10, n. 4, p. 39, doi. 10.3390/g10040039
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Geocentric Spherical Surfaces Emulating the Geostationary Orbit at Any Latitude with Zenith Links.
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- Future Internet, 2020, v. 12, n. 1, p. 16, doi. 10.3390/fi12010016
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Design and performance simulation of a satellite momentum exchange actuator.
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- Australian Journal of Mechanical Engineering, 2016, v. 14, n. 1, p. 1, doi. 10.1080/14484846.2015.1093223
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UAV attitude estimation based on MARG and optical flow sensors using gated recurrent unit.
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- International Journal of Distributed Sensor Networks, 2021, v. 17, n. 4, p. 1, doi. 10.1177/15501477211009814
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Efficient topology control for time-varying spacecraft networks with unreliable links.
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- International Journal of Distributed Sensor Networks, 2019, v. 15, n. 9, p. N.PAG, doi. 10.1177/1550147719879377
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Fault diagnosis method for closed-loop satellite attitude control systems based on a fuzzy parity equation.
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- International Journal of Distributed Sensor Networks, 2018, v. 14, n. 12, p. 1, doi. 10.1177/1550147718805938
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A rapid maneuver path planning method with complex sensor pointing constraints in the attitude space.
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- Information Systems Frontiers, 2017, v. 19, n. 4, p. 945, doi. 10.1007/s10796-016-9642-1
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Predicting Flight-Driving Attitudes through EEG-Based Models.
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- International Journal of Pattern Recognition & Artificial Intelligence, 2024, v. 38, n. 9, p. 1, doi. 10.1142/S0218001424590080
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Altitude and Attitude Stabilization of UAV Quadrotor System using Improved Active Disturbance Rejection Control.
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- Arabian Journal for Science & Engineering (Springer Science & Business Media B.V. ), 2020, v. 45, n. 3, p. 1985, doi. 10.1007/s13369-020-04355-3
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On the Influence of Sea Surface Height Variability on Satellite Altimeter Derived Gravity.
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- Marine Geodesy, 2001, v. 24, n. 2, p. 73, doi. 10.1080/014904101300182286
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On-orbit NOAA-20 VIIRS solar diffuser bidirectional reflectance distribution function and screen transmittance characterization using yaw manoeuvres and regular on-orbit SDSM data.
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- International Journal of Remote Sensing, 2020, v. 41, n. 17, p. 6503, doi. 10.1080/01431161.2020.1739353
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Monitoring of Dangerous Ice Phenomena Using Satellite Imagery and Model Simulation.
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- Russian Meteorology & Hydrology, 2019, v. 44, n. 11, p. 746, doi. 10.3103/S1068373919110049
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Multimotors Coordination Control Method for Consistent Total Traction Torque of Electric Locomotives.
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- Journal of Advanced Transportation, 2020, p. 1, doi. 10.1155/2020/2092463
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Antimicrobial Photoinactivation Approach Based on Natural Agents for Control of Bacteria Biofilms in Spacecraft.
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- International Journal of Molecular Sciences, 2020, v. 21, n. 18, p. 6932, doi. 10.3390/ijms21186932
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Optimal cooperative control for formation flying spacecraft with collision avoidance.
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- Science Progress, 2019, v. 103, n. 1, p. 1, doi. 10.1177/0036850419884432
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The pointing system of the Herschel space observatory.
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- Experimental Astronomy, 2014, v. 37, n. 2, p. 453, doi. 10.1007/s10686-014-9396-z
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Reliability evaluation of phased mission system under multiple correlated failure modes.
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- Quality & Reliability Engineering International, 2023, v. 39, n. 8, p. 3266, doi. 10.1002/qre.3122
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Controller design by using non-linear control methods for satellite chaotic system.
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- Electrical Engineering, 2017, v. 99, n. 2, p. 763, doi. 10.1007/s00202-016-0450-x
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A Detection Method for the Random Noise Failure of Mems Gyros on Orbit.
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- Russian Physics Journal, 2022, v. 64, n. 10, p. 1857, doi. 10.1007/s11182-022-02526-3
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Appointed‐time nonsingular sliding mode control of spacecraft attitude stabilization.
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- IET Control Theory & Applications (Wiley-Blackwell), 2023, v. 17, n. 14, p. 1944, doi. 10.1049/cth2.12516
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Optimal attitude consensus control for rigid spacecraft formation based on control Lyapunov functions.
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- IET Control Theory & Applications (Wiley-Blackwell), 2023, v. 17, n. 12, p. 1720, doi. 10.1049/cth2.12513
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Prescribed performance fault‐tolerant attitude control for flexible spacecraft under limited communication network.
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- IET Control Theory & Applications (Wiley-Blackwell), 2023, v. 17, n. 11, p. 1566, doi. 10.1049/cth2.12493
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