File:Navigation Constant illustration.png
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Summary
| Description | 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. |
| Date | |
| Source | Own work |
| Author | User:Skorkmaz |
Licensing
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I, the copyright holder of this work, release this work into the public domain. This applies worldwide. In some countries this may not be legally possible; if so: I grant anyone the right to use this work for any purpose, without any conditions, unless such conditions are required by law. |
File history
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 08:16, 26 April 2008 | | 206 × 197 (3 KB) | Skorkmaz | {{Information |Description= |Source= |Date= |Author= |Permission= |other_versions= }} |
| 07:38, 26 April 2008 |  | 184 × 182 (3 KB) | Skorkmaz | {{Information |Description= |Source= |Date= |Author= |Permission= |other_versions= }} |
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