A method and apparatus for the control of the attitude of earth orbiting satellites and the orbit and attitude control of a novel gravitational wave detection satellite configuration located near the sun-earth Lagrangian points L3, L4 and L5, utilizing the control of solar radiation pressure by the use of electrically controllable variable reflection glass panels to provide the torques and forces needed.
Satellite control system using electrically controllable variable reflection glass panels
2020-05-12
Patent
Elektronische Ressource
Englisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
SATELLITE CONTROL SYSTEM USING ELECTRICALLY CONTROLLABLE VARIABLE REFLECTION GLASS PANELS
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