Method of the Autonomous Indirect Identification of the Conversion Factor of Pendulum Compensating Accelerometer Under the Conditions for the Orbital Flight of Automatic Spacecraft

Is examined the method of the autonomous indirect identification of the conversion factor of pendulum compensating accelerometer, which makes it possible with the high accuracy to determine the coefficient under the conditions for orbital flight indicated by the built-in firmware means of this gauge and to, thus, decrease an error in the determination of increase in the apparent in the velocity with the accomplishment of maneuver by automatic spacecraft