Event-triggered attitude tracking for rigid spacecraft

This study aims to investigate the problem of attitude control for a spacecraft with inertial uncertainties, external disturbances, and communication restrictions. An event-triggered active disturbance rejection control approach is proposed for attitude tracking of the spacecraft. An event-triggered...

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Veröffentlicht in:	Science China. Information sciences 2019-12, Vol.62 (12), p.222202, Article 222202
Hauptverfasser:	Cai, Deheng, Zou, Hengguang, Wang, Junzheng, Huang, Yuan, Shi, Dawei
Format:	Artikel
Sprache:	eng
Schlagworte:	Active control Communication Computer Science Design Disturbances Information Systems and Communication Service Investigations Kinematics Research Paper Spacecraft attitude control Spacecraft tracking State observers Tracking control Tracking systems
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