A gyroscopic pendulum used as an attitude indicator is characterized by the following parameters: mass of the gyroscope flywheel m = 5 • 103 g, moment of inertia of the flywheel relative to the axis of the figure I = 8 • 104 g•cm2, distance between the suspension point and the center of mass of the flywheel l = 10.25 cm. The gyroscope makes 20,000 rpm. When the plane on which the device was installed moved uniformly, the axis of the pendulum figure was vertical. Then, for a time t = 10 s, the plane moved with horizontal acceleration

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