Invention Grant
- Patent Title: Guidance system with varying error correction gain
- Patent Title (中): 引导系统具有不同的纠错增益
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Application No.: US11968705Application Date: 2008-01-03
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Publication No.: US07795565B2Publication Date: 2010-09-14
- Inventor: Gregory F. Bock
- Applicant: Gregory F. Bock
- Applicant Address: US MD Bethesda
- Assignee: Lockheed Martin Corporation
- Current Assignee: Lockheed Martin Corporation
- Current Assignee Address: US MD Bethesda
- Agency: Duane Morris LLP
- Main IPC: F41G7/22
- IPC: F41G7/22 ; F42B15/01 ; F41G7/00 ; F42B15/00

Abstract:
A guided missile or projectile and associated guidance control are provided to control a path to a point of intersection with a potentially moving target. A new path is repetitively recomputed and acceleration orthogonal to the path is applied to minimize heading error and thereby to converge on the target. The gain of the control function is partly proportional to heading error, but the gain is reduced approaching the point of convergence. In this way, the guidance control is more responsive to actual variance of the true heading error and is less responsive to random error in sensing the target heading, which random error would otherwise increase in its contribution to corrective guidance movements approaching the point of intersection.
Public/Granted literature
- US20090173820A1 GUIDANCE SYSTEM WITH VARYING ERROR CORRECTION GAIN Public/Granted day:2009-07-09
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