OPTIMIZATION OF HEMISPHERICAL RESONATOR GYROSCOPE STANDING WAVE PARAMETERS
Traditionally, the problem of autonomous navigation is solved by dead reckoning navigation flight parameters (NFP) of the aircraft (AC). With increasing requirements to accuracy of definition NFP improved the sensors of the primary navigation information: gyroscopes and accelerometers. the gyroscope...
Bewaard in:
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| Formaat: | Artigo |
| Taal: | Russo |
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Moscow State Technical University of Civil Aviation
2017-03-01
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| Reeks: | Научный вестник МГТУ ГА |
| Onderwerpen: | |
| Online toegang: | https://avia.mstuca.ru/jour/article/view/1051 |
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