Fully-Actuated System Approach Based Optimal Attitude Tracking Control of Rigid Spacecraft with Actuator Saturation

Research article (Journal of Systems Science and Complexity, 2022) · cited 43× · AI/ML
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Fully-Actuated System Approach Based Optimal Attitude Tracking Control of Rigid Spacecraft with Actuator Saturation

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Fully-Actuated System Approach Based Optimal Attitude Tracking Control of Rigid Spacecraft with Actuator Saturation is a scholarly article[1].

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APA 4ort.xyz Knowledge Graph. (2026). Fully-Actuated System Approach Based Optimal Attitude Tracking Control of Rigid Spacecraft with Actuator Saturation. Retrieved May 24, 2026, from https://4ort.xyz/entity/fully-actuated-system-approach-based-optimal-attitude-tracking-control-of-rigid-spacecraft-with-actuator-saturation
MLA “Fully-Actuated System Approach Based Optimal Attitude Tracking Control of Rigid Spacecraft with Actuator Saturation.” 4ort.xyz Knowledge Graph, 4ort.xyz, 24 May. 2026, https://4ort.xyz/entity/fully-actuated-system-approach-based-optimal-attitude-tracking-control-of-rigid-spacecraft-with-actuator-saturation.
BibTeX @misc{4ortxyz_fully-actuated-system-approach-based-optimal-attitude-tracking-control-of-rigid-spacecraft-with-actuator-saturation_2026, author = {{4ort.xyz Knowledge Graph}}, title = {{Fully-Actuated System Approach Based Optimal Attitude Tracking Control of Rigid Spacecraft with Actuator Saturation}}, year = {2026}, url = {https://4ort.xyz/entity/fully-actuated-system-approach-based-optimal-attitude-tracking-control-of-rigid-spacecraft-with-actuator-saturation}, note = {Accessed: 2026-05-24}}
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