An Application of a Special Method for Designating the Control Forces for the Homing of an Anti-Aircraft Missile on an Aerial Target by Use of a Method of Proportional Navigation
An analysis of application feasibility of a special method for surface-to-air missile (SAM) control during homing on an airborne target was carried out in this paper. A prior implementation of the method was motion control for a gyroscope axis with three degrees of freedom [1, 2] at the stages of sp...
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| Format: | Article |
| Language: | English |
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Military University of Technology, Warsaw, Poland
2018-12-01
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| Series: | Problemy Mechatroniki |
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| Online Access: | http://promechjournal.pl/gicid/01.3001.0012.7339 |