Application of an optimal control algorithm for a gyroscope system of a homing air-to-air missile
Missile homing precision depends mainly on the correct determination of the current angle between the Gyroscope System Axis (GSA) and the target line-of-sight (LOS). A gyroscope automatic control system shall ensure spontaneous levelling of this angle, hence, constant homing of the gyroscope system...
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| Format: | Article |
| Language: | English |
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Vilnius Gediminas Technical University
2021-04-01
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| Series: | Aviation |
| Subjects: | |
| Online Access: | https://journals.vgtu.lt/index.php/Aviation/article/view/13899 |