NDLI: Fuel optimal maneuver of circular-like satellite formation based on continuous low thrust

Content Provider	IEEE Xplore Digital Library
Author	Guangyan Xu Xiaoying Wang Ping Li Xia Chen
Copyright Year	2014
Description	Author affiliation: Sch. of Autom., Shenyang Aerosp. Univ., Shenyang, China (Guangyan Xu; Xiaoying Wang; Ping Li; Xia Chen)
Abstract	An effective method is proposed to formulate and solve a fuel-optimal control problem of satellite formation maneuver using continuous low thrusters. To ensure long-term flying formation and to save fuel practically possible, the final satellite formation is designed as the passive and periodic relative orbits accommodating the $J_{2}$ perturbation. Based on the conditions of the passive and periodic relative trajectory and combining with the unknown final injection time, a final orbit is described by six implicit constraint equations. In order to overcome the complex and difficult computation, the nonlinear optimal control problem is converted into a nonlinear programming problem by means of the Legendre pseudospectral method. Due to the formulated problem including the free final time and the precise final constraints, the formation maneuver is very reasonable and the fuel consumption is minimized. The numerical results show that the control law works well for the optimal reconfiguration of satellite formation.
Starting Page	9054
Ending Page	9059
File Size	185275
Page Count	6
File Format	PDF
ISBN	9789881563873
ISSN	19341768
DOI	10.1109/ChiCC.2014.6896525
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2014-07-28
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	TCCT, CAA
Subject Keyword	Formation Maneuver Nonlinear Fuel-optimal Control Nonlinear Programming Satellites Optimal control Legendre Pseudospectral Approach Orbits Trajectory Satellites Relative Motion Fuels Mathematical model Equations
Content Type	Text
Resource Type	Article

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