This chapter is focused to control of relative satellite vector estimations with various Kalman filter (KF) and Proportional-Integral-Derivative (PID) approaches. The identical 3U target and follower satellites orbits and initial conditions are simulated according with desired formation geometry limitations. In this study, target and follower satellites states are determined as derived simulation data. The various satellites thruster’s scenario is analyzed with various relative state estimation which use Kalman filters. The novel methods, which satellites and relative orbit estimation are determined via two stages, are inputted to the control section of follower satellites within formation flight of satellites architecture.


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    Title :

    Satellite Formation Flight via Thrusters and Proportional-Integral-Derivative Control Approaches


    Additional title:

    Sustainable aviat.



    Conference:

    International Symposium on Unmanned Systems and The Defense Industry ; 2021 ; Washington, DC, DC, USA October 26, 2021 - October 28, 2021



    Publication date :

    2023-06-28


    Size :

    8 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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