
Приведено описание методики определения положения метеорологической ракеты в пространстве. Информация о положении осей ракеты в полёте получается в результате анализа показаний датчика линейных ускорений. Предлагаемая методика позволяет снизить стоимость используемых бортовых измерительных систем. The paper describes the methodology for attitude determination of meteorological rockets in space. Information on the rocket axes attitude in flight is the result of the analysis of the sensor linear accelerations. The proposed method can reduce the cost of onboard measuring systems used. Безукладников Евгений Владимирович - инженер-конструктор ОАО «ОКБ «Новатор», г. Екатеринбург; main@okb-novator.ru. Bezukladnikov Evgeny Vladimirovich - design engineer of OSC «EDB «Novator», Yekaterinburg; main@okbnovator.ru. Разумов Артем Николаевич - техник-конструктор ОАО «ОКБ «Новатор», г. Екатеринбург; main@okbnovator.ru. Razumov Artem Nikolaevich - technical engineer of OSC «EDB «Novator», Yekaterinburg; main@okb-novator.ru
определение положения, определение ориентации., meteorological rocket, 006.91 [УДК 629.76.05], attitude determ, position determination, метеорологическая ракета
определение положения, определение ориентации., meteorological rocket, 006.91 [УДК 629.76.05], attitude determ, position determination, метеорологическая ракета
| selected citations These citations are derived from selected sources. This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically). | 0 | |
| popularity This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network. | Average | |
| influence This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically). | Average | |
| impulse This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network. | Average |
