A low-complexity attitude control method for large-angle agile maneuvers of a spacecraft with control moment gyros

Kawajiri, Shota; Matunaga, Saburo

doi:10.1016/j.actaastro.2017.07.039

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Cited by 10 publications

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“…Yu et al used H ∞ and composite control methods to achieve large-angle rapid maneuvering control of flexible spacecraft [16]. Ali [17] and Kawajiri [18] also proposed control methods for rapid maneuvering at large angles.…”

Section: Introductionmentioning

confidence: 99%

Research on Control of Stewart Platform Integrating Small Attitude Maneuver and Vibration Isolation for High-Precision Payloads on Spacecraft

Chi¹,

Ma²,

Wang³

et al. 2021

Aerospace

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The Stewart platform, a classical mechanism proposed as the parallel operation apparatus of robots, is widely used for vibration isolation in various fields. In this paper, a design integrating both small attitude control and vibration isolation for high-precision payloads on board satellites is proposed. Our design is based on a Stewart platform equipped with voice-coil motors (VCM) to provide control force over the mechanism. The coupling terms in the dynamic equations of the legs are removed as the total disturbance by the linear active disturbance rejection control (LADRC). Attitude maneuver and vibration isolation performance is verified by numerical simulations.

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Section: Introductionmentioning

confidence: 99%