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- W2373085216 abstract "A control method to form relative fly-orbit directly under finite thrust while the chaser was arriving at the vicinity of the target was put forward in this paper.Based on the modified equinoctial elements,the control problem was converted into a classical optimal control by variation.The terminal dynamic constraints were derived from relative dynamics,which was solved by the nonlinear programming.The model was established.The theoretical analysis and simulation results showed that this method was feasible.But to reduce the error caused by the disturbance,the guidance law during the forming of the relative flying should be studied." @default.
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- W2373085216 date "2007-01-01" @default.
- W2373085216 modified "2023-09-28" @default.
- W2373085216 title "Directly Forming Relative Fly-Around Orbit under Finite Thrust" @default.
- W2373085216 hasPublicationYear "2007" @default.
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