Abstract Since its launch on 20 May 2004, FORMOSAT-2 (FS2, Formosa satellite ♯2) has been operated on orbit for more than 9 years. It carries two payloads: the remote sensing instrument (RSI) for Earth observations and the imager of sprites and upper atmospheric lightning instrument (ISUAL) for the purpose of scientific observations. The RSI is operating at daytime while ISUAL is active at night-time. To meet both mission objectives simultaneously, the satellite operations planning has been more complicated. In order to maximize the usage of the on-board resources, the satellite attitude maneuver activities and power charge/discharge cycles have been scheduled cautiously in every detail. Under such fully engaged operations scenario and with a design life of 5 years, it is inevitable that the satellite encountered many anomalies, either permanent or temporary. In particular, one attitude gyro (totally four) and one reaction wheel (totally four) have been failed. This paper presents the major anomalies and resolutions in the past years. Many iterations and trade-offs have been made to minimize the effect on mission operations of the handicapped FORMOSAT-2. It still can provide about 80% of the designed functions and capabilities.

    Highlights Nine years after launch one attitude gyro and one reaction wheel of FORMOSAT-2 failed. The inertial reference unit had redundant design, failure of one gyro had no effect. Major analysis focused on the root cause and effect of the failure of reaction wheel. Root cause had been identified: failure between reaction wheel C and tele-command interface. About 80% of imaging capabilities of the handicapped FORMOSAT-2 are kept.


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    Title :

    Mission operations of the handicapped FORMOSAT-2


    Contributors:

    Published in:

    Acta Astronautica ; 103 ; 243-249


    Publication date :

    2014-06-03


    Size :

    7 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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