发明名称 |
Method and system for determining the attitude of an aircraft by multi-axial accelerometric measurements |
摘要 |
<p>The method involves determining an angle of pitch and/or an angle of heading and/or an angle of roll of an aircraft (100). A first pair of accelerometers (A5, A6) used for determination of the angle of heading is arranged on a side of a center of gravity (G) along an axis merged with a transverse axis of the aircraft. A second pair of accelerometers (A3, A4) used for determination of the angle of roll is arranged on a side of the center of gravity along a vertical axis (z) perpendicular to a plane formed by other axes (x, y). An independent claim is also included for an inertial navigation system.</p> |
申请公布号 |
EP2495530(B1) |
申请公布日期 |
2014.04.16 |
申请号 |
EP20120156798 |
申请日期 |
2012.02.24 |
申请人 |
THALES |
发明人 |
REVOL, MARC;MANDLE, JACQUES;BIBAUT, ALAIN;COATANTIEC, JACQUES |
分类号 |
G01C21/16;G05D1/08 |
主分类号 |
G01C21/16 |
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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