Test Mass Capture Control for Drag-Free Satellite Based on State-Dependent Riccati Equation Method

Yingjie Chen; Yankai Wang; Ti Chen; Zhengtao Wei; Javad Tayebi

doi:10.3390/act13110434

journal article Open Access Oct 27, 2024

Test Mass Capture Control for Drag-Free Satellite Based on State-Dependent Riccati Equation Method

Yingjie Chen

Yankai Wang

Ti Chen

Zhengtao Wei Javad Tayebi

Actuators Vol. 13 No. 11 pp. 434 · MDPI AG

View at Publisher Save 10.3390/act13110434

Abstract

The drag-free satellite plays an important role in the space-based gravitational wave observatory. The capture control of test mass after release is a crucial technology that can affect the success of the mission. The test mass must be released to the center of the electrostatic suspension cage accurately. This paper presents a nonlinear dynamic model of drag-free satellites in Lagrange formalism. A capture control scheme for test mass release phase is proposed based on the state-dependent Riccati equation (SDRE) strategy. To deal with the actuator saturation problem, a nonlinear saturation model is introduced to the dynamics of satellite, while the SDRE strategy is applied to the non-affine system. The effectiveness of the proposed methodology is verified by the numerical simulation for the drag-free satellite.

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Published: Oct 27, 2024
Vol/Issue: 13(11)
Pages: 434
License: View

Authors

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Yingjie Chen