In many unmanned aerial vehicle (UAV) applications, achieving stable flight despite actuator failures is crucial. Among the many existing fault-tolerant control (FTC) methods, adaptive control is a practical approach.
Yasuyuki Satoh, Anan Tabata
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CFHBA-PID Algorithm: Dual-Loop PID Balancing Robot Attitude Control Algorithm Based on Complementary Factor and Honey Badger Algorithm. [PDF]
Lin J +5 more
europepmc +1 more source
Condensing AI-Based Attitude Control Using Kolmogorov–Arnold Networks for Memory Efficiency
Artificial Intelligence (AI) is rapidly transforming engineering fields, from robotics to aerospace, with applications in control systems for UAVs and satellites.
Kirill Djebko +4 more
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Design of an Attitude Control System for a Stereo-Imagery Satellite with Combining of Along-Track and Across-Track Configurations [PDF]
In this paper, the main stereo-imaging methods by high resolution satellites, including Along-Track and Across-Track, have been evaluated and then we will combine the two main stereo-imaging configurations of along track and across track as a new idea to
H. Bolandi +2 more
doaj
This work investigates the attitude stabilization and synchronization problem for multi-combined spacecraft with time-varying inertia parameters, external disturbances, and input constraints.
Xianglong Kong +3 more
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Attitude Control of Over-Actuated Fixed-Wing Aircraft Based on Predefined Time Control
This paper presents a novel predefined-time attitude-control framework for fixed-wing aircraft with over-actuated systems, solving aerodynamic uncertainties and nonlinear couplings during high-angle-of-attack flight. The proposed methodology integrates a
Fangping Chen +8 more
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Attitude Maneuver Control of Rigid Spacecraft Based on Model-Free Controller Guide SAC Algorithm
This paper presents a model-free attitude control algorithm applied to rigid spacecraft. The Soft Actor–Critical (SAC) deep reinforcement learning algorithm is initially employed for spacecraft control, and two modifications are proposed to address the ...
Di Huang, Xiangkun Li, Zekun Zhu
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A new type of six-rotor and its attitude active disturbance rejection realization
Based on the traditional four-rotor configuration, the new six-rotor adds two main thrust propellers, which can fly forward quickly without changing the pitch angle and realize yaw quickly.
LI Yaoqiang, XU Jinfa
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Usability evaluation of attitude control for a robotic wheelchair for tip mitigation in outdoor environments. [PDF]
Sivakanthan S +9 more
europepmc +1 more source
Variable-Structure Near-Space Vehicles with Time-Varying State Constraints Attitude Control Based on Switched Nonlinear System. [PDF]
Feng C, Wang Q, Liu C, Hu C, Liang X.
europepmc +1 more source

