发明申请
US20060053887A1 Generalized inertial measurement error reduction through multiple axis rotation during flight 有权
飞行过程中通过多轴旋转的广义惯性测量误差减少

  • 专利标题: Generalized inertial measurement error reduction through multiple axis rotation during flight
  • 专利标题(中): 飞行过程中通过多轴旋转的广义惯性测量误差减少
  • 申请号: US11004517
    申请日: 2004-12-03
  • 公开(公告)号: US20060053887A1
    公开(公告)日: 2006-03-16
  • 发明人: Robert Fall
  • 申请人: Robert Fall
  • 申请人地址: US NJ MORRISTOWN
  • 专利权人: HONEYWELL INTERNATINAL INC.
  • 当前专利权人: HONEYWELL INTERNATINAL INC.
  • 当前专利权人地址: US NJ MORRISTOWN
  • 主分类号: G01C21/12
  • IPC分类号: G01C21/12 G01C25/00 G01P15/18
Generalized inertial measurement error reduction through multiple axis rotation during flight
摘要:
An inertial measurement unit is provided. The inertial measurement unit comprises two rotational axes, wherein a first of the two rotational axes is aligned nominally along a thrust axis and a second of the two rotational axes is aligned substantially perpendicular to a plane formed by a local gravity vector and a thrust vector, and one or more sensors which rotate about the second rotational axis.
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