Attitude Control using only Magnetorquers for a Sun-Pointing Mission
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1
Attitude Control using only Magnetorquers for a Sun-Pointing Mission
~EN NW ABISBN: 9783639850116 bzw. 3639850114, vermutlich in Englisch, VDM Verlag Dr. Müller, Saarbrücken, Deutschland, neu, Hörbuch.
Lieferung aus: Schweiz, Lieferzeit: 2 Tage, zzgl. Versandkosten.
The interest in adopting magnetic actuators for attitude control, i.e. in using the interaction between the geomagnetic field and the on board magnetorquers, increases as the interest in small satellites rises. In fact magnetic control is a valid choice for missions in which satellites have a low weight and have no sub-degree requirement for pointing accuracy. To have an efficient control, satellites in quasi-polar Low Earth Orbit have to be considered: quasi-polar orbit is justified from the particular structure of the geomagnetic field (in fact in an equatorial or less inclined orbit the components of the geomagnetic field result quasi-constant and it can be very difficult to achieve any attitude maneuver), LEO is necessary because the influence of the geomagnetic field is significant only in a range of altitudes near to the Earth. The primary purpose of this work is to extend the application of a three-axis magnetic control to different types of missions, which satisfy the previous restrictions, in particular to Sun-pointing missions. Similar works in the literature are based on a nadir-pointing attitude, aided by a gravity gradient stabilization (see Psiaki and Wisniewsy).
The interest in adopting magnetic actuators for attitude control, i.e. in using the interaction between the geomagnetic field and the on board magnetorquers, increases as the interest in small satellites rises. In fact magnetic control is a valid choice for missions in which satellites have a low weight and have no sub-degree requirement for pointing accuracy. To have an efficient control, satellites in quasi-polar Low Earth Orbit have to be considered: quasi-polar orbit is justified from the particular structure of the geomagnetic field (in fact in an equatorial or less inclined orbit the components of the geomagnetic field result quasi-constant and it can be very difficult to achieve any attitude maneuver), LEO is necessary because the influence of the geomagnetic field is significant only in a range of altitudes near to the Earth. The primary purpose of this work is to extend the application of a three-axis magnetic control to different types of missions, which satisfy the previous restrictions, in particular to Sun-pointing missions. Similar works in the literature are based on a nadir-pointing attitude, aided by a gravity gradient stabilization (see Psiaki and Wisniewsy).
2
Attitude Control using only Magnetorquers for a Sun-Pointing Mission - Study of a Three-Axis Stabilized Satellite
~EN PB NWISBN: 9783639850116 bzw. 3639850114, vermutlich in Englisch, Edizioni Accademiche Italiane, Taschenbuch, neu.
Lieferung aus: Deutschland, Versandkostenfrei.
Attitude Control using only Magnetorquers for a Sun-Pointing Mission: The interest in adopting magnetic actuators for attitude control, i.e. in using the interaction between the geomagnetic field and the on board magnetorquers, increases as the interest in small satellites rises. In fact magnetic control is a valid choice for missions in which satellites have a low weight and have no sub-degree requirement for pointing accuracy. To have an efficient control, satellites in quasi-polar Low Earth Orbit have to be considered: quasi-polar orbit is justified from the particular structure of the geomagnetic field (in fact in an equatorial or less inclined orbit the components of the geomagnetic field result quasi-constant and it can be very difficult to achieve any attitude maneuver) LEO is necessary because the influence of the geomagnetic field is significant only in a range of altitudes near to the Earth. The primary purpose of this work is to extend the application of a three-axis magnetic control to different types of missions, which satisfy the previous restrictions, in particular to Sun-pointing missions. Similar works in the literature are based on a nadir-pointing attitude, aided by a gravity gradient stabilization (see Psiaki and Wisniewsy). Englisch, Taschenbuch.
Attitude Control using only Magnetorquers for a Sun-Pointing Mission: The interest in adopting magnetic actuators for attitude control, i.e. in using the interaction between the geomagnetic field and the on board magnetorquers, increases as the interest in small satellites rises. In fact magnetic control is a valid choice for missions in which satellites have a low weight and have no sub-degree requirement for pointing accuracy. To have an efficient control, satellites in quasi-polar Low Earth Orbit have to be considered: quasi-polar orbit is justified from the particular structure of the geomagnetic field (in fact in an equatorial or less inclined orbit the components of the geomagnetic field result quasi-constant and it can be very difficult to achieve any attitude maneuver) LEO is necessary because the influence of the geomagnetic field is significant only in a range of altitudes near to the Earth. The primary purpose of this work is to extend the application of a three-axis magnetic control to different types of missions, which satisfy the previous restrictions, in particular to Sun-pointing missions. Similar works in the literature are based on a nadir-pointing attitude, aided by a gravity gradient stabilization (see Psiaki and Wisniewsy). Englisch, Taschenbuch.
3
Attitude Control using only Magnetorquers for a Sun-Pointing Mission: Study of a Three-Axis Stabilized Satellite (2014)
EN PB USISBN: 9783639850116 bzw. 3639850114, in Englisch, 144 Seiten, Edizioni Accademiche Italiane, Taschenbuch, gebraucht.
Neu ab: $46.97 (10 Angebote)
Gebraucht ab: $49.53 (5 Angebote)
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Von Händler/Antiquariat, Wordery USA.
The interest in adopting magnetic actuators for attitude control, i.e. in using the interaction between the geomagnetic field and the on board magnetorquers, increases as the interest in small satellites rises. In fact magnetic control is a valid choice for missions in which satellites have a low weight and have no sub-degree requirement for pointing accuracy. To have an efficient control, satellites in quasi-polar Low Earth Orbit have to be considered: quasi-polar orbit is justified from the particular structure of the geomagnetic field (in fact in an equatorial or less inclined orbit the components of the geomagnetic field result quasi-constant and it can be very difficult to achieve any attitude maneuver); LEO is necessary because the influence of the geomagnetic field is significant only in a range of altitudes near to the Earth. The primary purpose of this work is to extend the application of a three-axis magnetic control to different types of missions, which satisfy the previous restrictions, in particular to Sun-pointing missions. Similar works in the literature are based on a nadir-pointing attitude, aided by a gravity gradient stabilization (see Psiaki and Wisniewsy). Paperback, Label: Edizioni Accademiche Italiane, Edizioni Accademiche Italiane, Produktgruppe: Book, Publiziert: 2014-04-25, Freigegeben: 2014-04-25, Studio: Edizioni Accademiche Italiane, Verkaufsrang: 5638098.
Von Händler/Antiquariat, Wordery USA.
The interest in adopting magnetic actuators for attitude control, i.e. in using the interaction between the geomagnetic field and the on board magnetorquers, increases as the interest in small satellites rises. In fact magnetic control is a valid choice for missions in which satellites have a low weight and have no sub-degree requirement for pointing accuracy. To have an efficient control, satellites in quasi-polar Low Earth Orbit have to be considered: quasi-polar orbit is justified from the particular structure of the geomagnetic field (in fact in an equatorial or less inclined orbit the components of the geomagnetic field result quasi-constant and it can be very difficult to achieve any attitude maneuver); LEO is necessary because the influence of the geomagnetic field is significant only in a range of altitudes near to the Earth. The primary purpose of this work is to extend the application of a three-axis magnetic control to different types of missions, which satisfy the previous restrictions, in particular to Sun-pointing missions. Similar works in the literature are based on a nadir-pointing attitude, aided by a gravity gradient stabilization (see Psiaki and Wisniewsy). Paperback, Label: Edizioni Accademiche Italiane, Edizioni Accademiche Italiane, Produktgruppe: Book, Publiziert: 2014-04-25, Freigegeben: 2014-04-25, Studio: Edizioni Accademiche Italiane, Verkaufsrang: 5638098.
4
Attitude Control using only Magnetorquers for a Sun-Pointing Mission
~EN NWISBN: 3639850114 bzw. 9783639850116, vermutlich in Englisch, VDM Verlag Dr. Müller, Saarbrücken, Deutschland, neu.
Attitude Control using only Magnetorquers for a Sun-Pointing Mission ab 36.9 EURO Study of a Three-Axis Stabilized Satellite.
5
Attitude Control using only Magnetorquers for a Sun-Pointing Mission
~EN PB NWISBN: 3639850114 bzw. 9783639850116, vermutlich in Englisch, Edizioni Accademiche Italiane, Taschenbuch, neu.
Attitude Control using only Magnetorquers for a Sun-Pointing Mission ab 36.9 € als Taschenbuch: Study of a Three-Axis Stabilized Satellite. Aus dem Bereich: Bücher, Wissenschaft, Technik,.
6
Attitude Control using only Magnetorquers for Su (2014)
~EN PB NWISBN: 9783639850116 bzw. 3639850114, vermutlich in Englisch, VDM Verlag Dr. Müller, Saarbrücken, Deutschland, Taschenbuch, neu.
Lieferung aus: Deutschland, Next Day, Versandkostenfrei.
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7
NEW Attitude Control Using Only Magnetorquers. BOOK (Paperback / softback)
DE NWISBN: 9783639850116 bzw. 3639850114, in Deutsch, VDM Verlag Dr. Müller, Saarbrücken, Deutschland, neu.
Lieferung aus: Vereinigte Staaten von Amerika, Lieferart: Free, Lieferung: Europe, Artikelstandort: USA, Versandkostenfrei.
Von Händler/Antiquariat, grey_elk_books_au_and_uk - Grey Elk Books.
Festpreisangebot.
Von Händler/Antiquariat, grey_elk_books_au_and_uk - Grey Elk Books.
Festpreisangebot.
8
Mauta, A: Attitude Control using only Magnetorquers for a Su #I#
DE NWISBN: 9783639850116 bzw. 3639850114, in Deutsch, VDM Verlag Dr. Müller, Saarbrücken, Deutschland, neu.
Lieferung aus: Deutschland, Lieferart: Free, Lieferung: Deutschland, Artikelstandort: Deutschland, Versandkostenfrei.
Von Händler/Antiquariat, averdo.
Festpreisangebot.
Von Händler/Antiquariat, averdo.
Festpreisangebot.
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