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- W2383037820 abstract "A linear model including J2 perturbation in the Cartesian coordinates is presented for spacecraft formation flight.The Lagrange method is used to obtain this model by including the absolute effect on the reference orbit and the relative effect on the relative motion of the formation satellites under the J2 perturbation.This model accounts for the short-period perturbation of the orbital radius of the reference satellite and the angular velocities of the chief-fixed rotating reference frame,which also does not neglect the coupling terms between the out-of-plane and in-plane equations,thus leading to the improvement of accuracy.A numerical simulation illustrates that the relative trajectory error of this model is only 10% with respect to the nonlinear two body propagator model,and the relative radius error of the projected circular formation is less than 1%.At the same time,the model is linear state space form that is convenient to design the guidance,navigation and control system in formation flight missions." @default.
- W2383037820 created "2016-06-24" @default.
- W2383037820 creator A5077398580 @default.
- W2383037820 date "2013-01-01" @default.
- W2383037820 modified "2023-09-28" @default.
- W2383037820 title "Linearized Formation Flight Dynamics Model under J_2 Perturbation" @default.
- W2383037820 hasPublicationYear "2013" @default.
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