FIELD: space engineering; semi-passive control systems of artificial earth satellites. SUBSTANCE: double electrostatic layer is applied on part of surface of artificial earth satellite for control of its orientation. During interaction of this layer with earth magnetic field, control moment of Lorenz forces arises which has orientation effect on artificial earth satellite. For steady orientation of artificial earth satellite, magnitude and direction of vector of dipole moment of double layer is changed in orbital coordinate system with gravitational disturbances taken into account, thus making it possible to solve problem of stabilization of artificial earth satellite at presence of dampening. For realization of controllable double electrostatic layer, use is made of system of controllable power supply sources and electrodes arranged on insulating struts on the outside of conducting envelope of artificial earth satellite forming double electric layer with controllable distribution of polarization together with it. Power supply sources are insulated from conducting envelope of artificial earth satellite and are controlled via fiber-optics lines in three mutually perpendicular axes. EFFECT: extended filed of application; enhanced compatibility with scientific equipment of artificial earth satellite. 4 cl, 7 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF SEMI-PASSIVE THREE-AXIS STABILISATION OF DYNAMICALLY SYMMETRIC ARTIFICIAL EARTH SATELLITE | 2006 |
|
RU2332334C1 |
METHOD OF CONTROL OF ARTIFICIAL SATELLITE ORIENTATION | 1998 |
|
RU2159201C2 |
DAMPING DEVICE FOR STABILIZATION OF ELECTRODYNAMIC ROPE SYSTEM | 2018 |
|
RU2709295C1 |
DEVICE OF STABILIZATION OF ELECTRODYNAMIC CABLE SYSTEM FOR REMOVING SPACE WASTE | 2017 |
|
RU2666610C1 |
METHOD FOR ORIENTATION OF NEAR-EARTH ORBITING SPACECRAFT | 2021 |
|
RU2779658C1 |
METHOD OF ORIENTATION AND ATTITUDE CONTROL SYSTEM FOR REALIZATION OF THIS METHOD | 1999 |
|
RU2150412C1 |
METHOD FOR ELECTROMAGNETIC DISPOSAL OF ELECTRICALLY CONDUCTIVE SPACE DEBRIS IN THE NEAR-EARTH SPACE AND APPARATUS FOR NON-CONTACT CAPTURING AND RETENTION OF ONE OR MORE ELECTRICALLY CONDUCTIVE ITEMS OF SPACE DEBRIS | 2020 |
|
RU2769807C1 |
METHOD AND DEVICE FOR MAGNETIC RELIEF OF INTERNAL ACTUATORS OF SPACE VEHICLE | 1992 |
|
RU2070148C1 |
METHOD OF DETECTING MAGNETIC INTERFERENCE IN SPACECRAFT IN FLIGHT | 2009 |
|
RU2408507C1 |
METHOD OF DETERMINING SPACECRAFT THREE-AXIS ORIENTATION | 2009 |
|
RU2408508C1 |
Authors
Dates
2002-10-20—Published
2001-03-16—Filed