File:Navigation Constant illustration.png

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Navigation_Constant_illustration.png(206 × 197 pixels, file size: 3 KB, MIME type: image/png)

Summary

For example, if the line of sight rotates slowly from north to east, the missile should turn to the right by a certain factor faster than the LOS-rate. This factor is N. User:Skorkmaz - Own work Proportional navigation guidance in missiles enables them to pursue targets, applying a steering correction proportional to the error in heading between the missile and the target.

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Date/TimeThumbnailDimensionsUserComment
current08:49, 20 July 2023Thumbnail for version as of 08:49, 20 July 2023206 × 197 (3 KB)Isidore (talk | contribs)For example, if the line of sight rotates slowly from north to east, the missile should turn to the right by a certain factor faster than the LOS-rate. This factor is N. User:Skorkmaz - Own work Proportional navigation guidance in missiles enables them to pursue targets, applying a steering correction proportional to the error in heading between the missile and the target.

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