OPTIMAL STRATEGIES FOR ORBITAL INCLINATION CONTROL OF GEOSTATIONARY SATELLITE

Abstract

Abstract: Using inclination vector as a non-singular orbital element, engineering oriented mathematical models for inclination control of geosta- tionary orbit are established,and unified optimal strategies for inclination control both in north-south station aquisition and north-south station keeping derived.The results are applicable to the missions which require north-south station keeping accuracy of 0.05°～0.1° and have been implemented in flight control of the Chinese STW-2 satellite.

Key words: Geosynchronous orbit, Orbital control, Optimal strategy

Li Tieshou Beijing Institute of Control Engineering. OPTIMAL STRATEGIES FOR ORBITAL INCLINATION CONTROL OF GEOSTATIONARY SATELLITE[J]. .

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OPTIMAL STRATEGIES FOR ORBITAL INCLINATION CONTROL OF GEOSTATIONARY SATELLITE

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