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...

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第一著者:	O. S. Khalyutina
フォーマット:	Artigo
言語:	Russo
出版事項:	Moscow State Technical University of Civil Aviation 2017-03-01
シリーズ:	Научный вестник МГТУ ГА
主題:	hemispherical resonator gyroscope (hrg) measurement accuracy optimal control the concept of inverse problems of dynamics
オンライン･アクセス:	https://avia.mstuca.ru/jour/article/view/1051
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