发明名称 Inertial navigation system error correction
摘要 Methods and apparatus for: (a) the correction of one or more elements determined from a first set of continuous gyro and accelerometer measurements comprising using a second set of discontinuously measured higher accuracy accelerometer measurements doubly integrated in an inertial coordinate system, (b) determining relative movement of a vehicle using a first set of acceleration measurements that do not include components of acceleration caused by the Earth's gravitational field, and a second set of acceleration measurements that do include components of acceleration caused by the Earth's gravitational field; and (c) correcting errors in an inertial navigation system positioned in a vehicle comprising using independently measured changes in position of the vehicle relative to an inertial coordinate frame.
申请公布号 US8311739(B2) 申请公布日期 2012.11.13
申请号 US20090362383 申请日期 2009.01.29
申请人 HUDDLE JAMES R.;NORTHROP GRUMMAN GUIDANCE AND ELECTRONICS COMPANY, INC. 发明人 HUDDLE JAMES R.
分类号 G01C21/00;G01C21/10;G01C21/16;G01C25/00;G01S19/53;G08G1/0969 主分类号 G01C21/00
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