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• W2016078703 abstract "Observer-based hovering control over a tumbling asteroid in the body-fixed frame is studied. An extended Kalman filter (EKF) is used to process range measurements from a small collection of ground stations, yielding estimates of the spacecraft state vector and the gravitational parameters of the asteroid assuming a second degree and order gravity field model. The estimated states are used in the optimal feedback control algorithm which consists of two alternatives: time-varying LQR or the Lyapunov–Floquet transformation (LFT) and time-invariant LQR. The closed-loop response of the system and the control effort required are investigated and compared for both control strategies." @default.
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• W2016078703 date "2014-09-01" @default.
• W2016078703 modified "2023-09-27" @default.
• W2016078703 title "Observer-based body-frame hovering control over a tumbling asteroid" @default.
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• W2016078703 doi "https://doi.org/10.1016/j.actaastro.2014.05.016" @default.
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