Тр. СПИИРАН
 2015
DOI: 10.15622/sp.40.7
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Method of the Autonomous Indirect Identification of the Conversion Factor of Pendulum Compensating Accelerometer Under the Conditions for the Orbital Flight of Automatic Spacecraft

Вячеслав Иванович Миронов1,
И. В. Фоминов2,
A.N. Maletin3
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