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RQP Based Finite Thrust Apogee Orbit Transfer with Minimum Fuel
Pages: 23-28
Year: Issue:  2
Journal: Aerospace Control

Keyword:  Communication satellite Orbital control Parameter optimization;
Abstract: In the view of the engineering, analyses the optimal apogee orbit transfer for geostationary satellites and defines the objective function, constraint conditions and the optimized parameters. According to the nature of the problem, uses the RQP method to find the optimzed parameters in orbit transfer and demonstrates the validity of the method by an engineering example.
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