Invention Grant
- Patent Title: Coning compensation in strapdown inertial navigation systems
- Patent Title (中): 在捷联惯性导航系统中进行补偿
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Application No.: US937251Application Date: 1997-07-01
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Publication No.: US5828980APublication Date: 1998-10-27
- Inventor: Daniel A. Tazartes , John G. Mark
- Applicant: Daniel A. Tazartes , John G. Mark
- Applicant Address: CA Woodland Hills
- Assignee: Litton Systems, Inc.
- Current Assignee: Litton Systems, Inc.
- Current Assignee Address: CA Woodland Hills
- Main IPC: G01C21/16
- IPC: G01C21/16 ; G05D1/00
Abstract:
The invention is a method for compensating for coning in a strapdown inertial navigation system which utilizes groups of five successive incremental angles of rotation of a body-fixed coordinate system as measured by orthogonally-mounted gyros at regular measurement intervals, each group of five measurements being obtained during a group interval equal to five measurement intervals. The coning-compensated angular displacement of the body-fixed coordinate system about a fixed axis in space during a p'th group interval is obtained by summing the five measured incremental angles and a coning compensation term. The coning compensation term consists of the sum of: (1) one-half the cross-product of a first and a second vector sum, the second vector sum being the sum of the five incremental angles of rotation in a group and the first vector sum being the sum of the second vector sum over p groups; and (2) the weighted sum of three vector cross-products, the multiplier and the multiplicand of each vector cross-product being a weighted sum of five measured incremental angles. The coning-compensated angular displacement can be summed over p to obtain an accurate estimate of the vector angle of rotation over a plurality of group intervals.
Public/Granted literature
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