Works matching DE "ARTIFICIAL satellite attitude control systems"
Results: 900
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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Finite-time fault-tolerant control of attitude control system of quadrotor UAV based on neural network disturbance observer.
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- Neural Computing & Applications, 2025, v. 37, n. 7, p. 5597, doi. 10.1007/s00521-024-10927-3
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Research on the Attitude Control Strategy of TBM Digging with V-Shaped Propulsion System.
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- Applied Sciences (2076-3417), 2025, v. 15, n. 4, p. 2244, doi. 10.3390/app15042244
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Angular Momentum Control Strategy of Control Moment Gyroscope Array Based on Deep Reinforcement Learning in Spacecraft Attitude Control System.
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- Aerospace (MDPI Publishing), 2025, v. 12, n. 2, p. 134, doi. 10.3390/aerospace12020134
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Attitude control of flexible satellite via three-dimensional magnetically suspended wheel.
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- Applied Mathematics & Mechanics, 2025, v. 46, n. 3, p. 555, doi. 10.1007/s10483-025-3232-7
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Towards a sustainable exploitation of the geosynchronous orbital region.
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- Celestial Mechanics & Dynamical Astronomy, 2019, v. 131, n. 4, p. N.PAG, doi. 10.1007/s10569-019-9895-3
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Attitude stability of a spacecraft on a stationary orbit around an asteroid subjected to gravity gradient torque.
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- Celestial Mechanics & Dynamical Astronomy, 2013, v. 115, n. 4, p. 333, doi. 10.1007/s10569-012-9463-6
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A modified between‐receiver single‐difference‐based fault detection and exclusion algorithm for real‐time kinematic positioning.
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- IET Radar, Sonar & Navigation (Wiley-Blackwell), 2022, v. 16, n. 8, p. 1269, doi. 10.1049/rsn2.12259
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Sizing design and implementation of a flywheel energy storage system for space applications.
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- Turkish Journal of Electrical Engineering & Computer Sciences, 2016, v. 24, n. 3, p. 793, doi. 10.3906/elk-1306-206
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Conceptual design of a low-cost real-time hardware-in-the-loop simulator for satellite attitude control system.
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- Turkish Journal of Electrical Engineering & Computer Sciences, 2015, v. 23, n. 3, p. 789, doi. 10.3906/elk-1212-20
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Performance evaluation of a fuzzy variable structure satellite attitude controller under sensor data delay.
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- Turkish Journal of Electrical Engineering & Computer Sciences, 2014, v. 22, n. 3, p. 517, doi. 10.3906/elk-1209-86
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A control algorithm for a simple flywheel energy storage system to be used in space applications.
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- Turkish Journal of Electrical Engineering & Computer Sciences, 2013, v. 21, n. 5, p. 1328, doi. 10.3906/elk-1111-65
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Review on Attitude Determination and Control Methods for Satellite Emergency Recovery.
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- Transactions of Nanjing University of Aeronautics & Astronautics, 2024, v. 41, n. 1-6, p. 675, doi. 10.16356/j.1005-1120.2024.06.001
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Attitude Control of a Flexible Solar Power Satellite Using Self‑tuning Iterative Learning Control.
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- Transactions of Nanjing University of Aeronautics & Astronautics, 2022, v. 39, n. 4, p. 389, doi. 10.16356/j.1005-1120.2022.04.002
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Sliding Mode Fault Tolerant Attitude Control Scheme for Spacecraft with Actuator Faults.
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- Transactions of Nanjing University of Aeronautics & Astronautics, 2019, v. 36, n. 1, p. 119, doi. 10.16356/j.1005-1120.2019.01.011
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Robust Coordinated Control for a Type of Hypersonic Aircraft.
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- Transactions of Nanjing University of Aeronautics & Astronautics, 2018, v. 35, n. 6, p. 1000, doi. 10.16356/j.1005-1120.2018.06.1000
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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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Method for control by orbital spacecraft magnetic cleanliness based on multiple magnetic dipole models with consideration of their uncertainty.
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- Electrical Engineering & Electromechanics, 2023, n. 5, p. 47, doi. 10.20998/2074-272X.2023.5.07
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Design of Optimal Intervention Based on a Generative Structural Causal Model.
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- Mathematics (2227-7390), 2024, v. 12, n. 20, p. 3172, doi. 10.3390/math12203172
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Optimal Synthesis of a Satellite Attitude Control System under Constraints on Control Torques and Velocities of Reaction Wheels.
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- Mathematics (2227-7390), 2024, v. 12, n. 16, p. 2569, doi. 10.3390/math12162569
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Finite-Time Extended State Observer-Based Attitude Control for Hypersonic Vehicles with Angle-of-Attack Constraint.
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- Mathematics (2227-7390), 2024, v. 12, n. 7, p. 1061, doi. 10.3390/math12071061
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Attitude Stabilization of a Satellite with Large Flexible Elements Using On-Board Actuators Only.
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- Mathematics (2227-7390), 2023, v. 11, n. 24, p. 4928, doi. 10.3390/math11244928
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Adaptive Sliding Mode Attitude Tracking Control for Rigid Spacecraft Considering the Unwinding Problem.
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- Mathematics (2227-7390), 2023, v. 11, n. 20, p. 4372, doi. 10.3390/math11204372
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Attitude Control of UAVs with Search Optimization and Disturbance Rejection Strategies.
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- Mathematics (2227-7390), 2023, v. 11, n. 17, p. 3794, doi. 10.3390/math11173794
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Hybrid Attitude Saturation and Fault-Tolerant Control for Rigid Spacecraft without Unwinding.
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- Mathematics (2227-7390), 2023, v. 11, n. 15, p. 3431, doi. 10.3390/math11153431
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Dynamics Analysis of a Nonlinear Satellite Attitude Control System Using an Exact Linear Model.
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- Mathematics (2227-7390), 2023, v. 11, n. 12, p. 2614, doi. 10.3390/math11122614
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Output Feedback Control for Spacecraft Attitude System with Practical Predefined-Time Stability Based on Anti-Windup Compensator.
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- Mathematics (2227-7390), 2023, v. 11, n. 9, p. 2149, doi. 10.3390/math11092149
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Finite-Time Contractive Control of Spacecraft Rendezvous System.
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- Mathematics (2227-7390), 2023, v. 11, n. 8, p. 1871, doi. 10.3390/math11081871
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Constrained Nonsingular Terminal Sliding Mode Attitude Control for Spacecraft: A Funnel Control Approach.
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- Mathematics (2227-7390), 2023, v. 11, n. 1, p. 247, doi. 10.3390/math11010247
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Tan-Type BLF-Based Attitude Tracking Control Design for Rigid Spacecraft with Arbitrary Disturbances.
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- Mathematics (2227-7390), 2022, v. 10, n. 23, p. 4548, doi. 10.3390/math10234548
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Attitude Control Method of Unmanned Helicopter Based on Asymmetric Tracking Differentiator and Fal-Extended State Observer.
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- Mathematics (2227-7390), 2022, v. 10, n. 19, p. 3439, doi. 10.3390/math10193439
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Finite-Time Extended State Observer-Based Fixed-Time Attitude Control for Hypersonic Vehicles.
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- Mathematics (2227-7390), 2022, v. 10, n. 17, p. 3162, doi. 10.3390/math10173162
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Indirect Neural-Enhanced Integral Sliding Mode Control for Finite-Time Fault-Tolerant Attitude Tracking of Spacecraft.
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- Mathematics (2227-7390), 2022, v. 10, n. 14, p. N.PAG, doi. 10.3390/math10142467
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North/South Station Keeping of the GEO Satellites in Asymmetric Configuration by Electric Propulsion with Manipulator.
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- Mathematics (2227-7390), 2022, v. 10, n. 13, p. 2340, doi. 10.3390/math10132340
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Event-Triggered Attitude-Orbit Coupled Fault-Tolerant Control for Multi-Spacecraft Formation.
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- Mathematics (2227-7390), 2022, v. 10, n. 12, p. 1984, doi. 10.3390/math10121984
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Neural Adaptive Fixed-Time Attitude Stabilization and Vibration Suppression of Flexible Spacecraft.
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- Mathematics (2227-7390), 2022, v. 10, n. 10, p. 1667, doi. 10.3390/math10101667
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Sliding Mode Controller Based on the Extended State Observer for Plant-Protection Quadrotor Unmanned Aerial Vehicles.
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- Mathematics (2227-7390), 2022, v. 10, n. 8, p. N.PAG, doi. 10.3390/math10081346
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An Adaptive Neuro-Fuzzy Model for Attitude Estimation and Control of a 3 DOF System.
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- Mathematics (2227-7390), 2022, v. 10, n. 6, p. 976, doi. 10.3390/math10060976
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Adaptive Sliding Mode Attitude-Tracking Control of Spacecraft with Prescribed Time Performance.
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- Mathematics (2227-7390), 2022, v. 10, n. 3, p. 401, doi. 10.3390/math10030401
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Attitude Control of a Flexible Spacecraft via Fuzzy Optimal Variance Technique †.
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- Mathematics (2227-7390), 2022, v. 10, n. 2, p. 179, doi. 10.3390/math10020179
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Robust Finite-Time Control Algorithm Based on Dynamic Sliding Mode for Satellite Attitude Maneuver.
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- Mathematics (2227-7390), 2022, v. 10, n. 1, p. 111, doi. 10.3390/math10010111
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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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- Article
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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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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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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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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