发明名称 |
Method and device for improving the inertial navigation of a projectile |
摘要 |
A method for the inertial navigation of a projectile equipped with a mediocre-quality inertial init that is fired from a carrier equipped with a precision inertial unit includes, before firing the projectile, the biases of the accelerometers and of the gyrometers of the inertial unit of the projectile are determined using the inertial unit of the carrier. During the inertial navigation of the projectile, the measurements of the accelermeters and of the gyrometers output by the inertial unit of the projectile are corrected by the biases determined before launching. |
申请公布号 |
US9534869(B2) |
申请公布日期 |
2017.01.03 |
申请号 |
US201414775260 |
申请日期 |
2014.03.12 |
申请人 |
MBDA FRANCE |
发明人 |
de Araujo Bruno;Guibout Vincent;Larcher Eric |
分类号 |
F41G7/36;G05D1/12;F41G7/00;G05D1/10;G01C21/16 |
主分类号 |
F41G7/36 |
代理机构 |
Christensen O'Connor Johnson Kindness PLLC |
代理人 |
Christensen O'Connor Johnson Kindness PLLC |
主权项 |
1. A method for improving the inertial navigation of a projectile equipped with a mediocre-quality inertial unit and fired from a carrier equipped with a precision inertial unit, comprising the following steps:
before firing the projectile from the carrier, determining mean biases of accelerometers and of gyrometers of the inertial unit of the projectile from the inertial unit of the carrier; firing the projectile from the carrier; inertially navigating the projectile while in flight with the inertial unit of the projectile, and during the inertial navigation of the projectile, correcting accelerometric and gyrometric measurements provided by the inertial unit of the projectile with the mean biases determined before firing. |
地址 |
Le Plessis-Robinson FR |