发明名称 |
METHOD OF CONTROLLING MAGNETIC TORQUERS OF AN ATTITUDE CONTROL SYSTEM OF A SPACECRAFT |
摘要 |
A method of command of magneto-torquers of an attitude control system of a space vehicle subjected to an external magnetic field of variable direction. The magneto-torquers are configured to desaturate an angular momentum storage device by transferring angular momentum and configured to form, in cooperation with the local external magnetic field, magnetic couples in a plane orthogonal to the direction of the local external magnetic field or a local control plane. The magnetic couple to be formed in the local control plane is determined as a function of the component of a desired attitude control couple which is orthogonal to the local control plane or a locally uncontrollable component. The contribution of the locally uncontrollable component to the magnetic couple to be formed is non-zero when the locally uncontrollable component is non-zero. |
申请公布号 |
EP2914497(B1) |
申请公布日期 |
2016.09.14 |
申请号 |
EP20130783329 |
申请日期 |
2013.10.25 |
申请人 |
AIRBUS DEFENCE AND SPACE SAS |
发明人 |
MORO, VALERIO |
分类号 |
B64G1/32;B64G1/24;B64G1/36;G01L3/10;G01L5/00;G01L5/22;G05D1/08 |
主分类号 |
B64G1/32 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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