NDLI: Low-Thrust Transfer Orbit Design Based on Lyapunov Feed Back Control Law

Content Provider	IEEE Xplore Digital Library
Author	Ren Yuan Cui Ping-yuan Luan En-jie
Copyright Year	2006
Description	Author affiliation: Deep Space Exploration Res. Center, Harbin Inst. of Technol. (Ren Yuan; Cui Ping-yuan)
Abstract	A novel low-thrust orbit transfer design method is presented which is based on the knowledge of optimal thrust direction and optimal location for changing each of the orbit elements and the concept of Lyapunov feedback control. In this method, a set of equinoctial elements is utilized to avoid the singularities in dynamical equation of classical orbit elements. A thruster switch law is derived by analyzing the effectivity of the changing of each orbit elements. The thrust will be cut-off if the effectivity is below a specified level. When on, the thrust is a constant. The two-body dynamics model is used in this method. The method needs few input parameters. By sequential quadratic programming (SQP), these parameters could be adjusted and performance index could be maximized. This method is a simple way to estimate key parameters of a low-thrust orbit transfer and could also give an accurate initial guesses for the future optimization
Starting Page	685
Ending Page	691
File Size	1889394
Page Count	7
File Format	PDF
ISBN	7302139229
DOI	10.1109/CESA.2006.4281740
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2006-10-04
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	IMACS
Subject Keyword	Design methodology Switches Lyapunov method Feedback control Quadratic programming Equations Space technology Lyapunov feedback control Optimal control Systems engineering and theory Feeds sequential quadratic programming low-thrust
Content Type	Text
Resource Type	Article

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