Inertial stabilizing system

Aeronautics and astronautics – Aircraft structure – Load accommodation

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Details

244 316, 248638, 348144, 348208, B64D 4708

Patent

active

054659248

ABSTRACT:
An inertial stabilizing system for a platform supported on a carrier, which is moved in a dynamically high-frequency and low-frequency manner, in which a base is arranged between the carrier and the platform which is mounted on the carrier so that it is vibration-insulated in a high-frequency manner via a damping device. On this base the platform is disposed in an adjustably movable manner by at least one control circuit which has an inertial sensor sensing the actual movements of the platform, a controller which forms an adjusting signal from the actual-desired value difference of the platform, and an adjusting device which is controlled by the adjusting signal and acts between the base and the platform. The control circuit has a further sensor which senses the low-frequency motion components of the damping device between the carrier and the base, and a control circuit element connected behind the sensor. For forming the control deviation, the control circuit element reduces the actual desired position difference in accordance with the sensor output signal, thereby considerably improving the interference and guiding behavior of the control circuit for abrupt changes of the desired value.

REFERENCES:
patent: 3617016 (1971-11-01), Bolsey
patent: 4245254 (1981-01-01), Svensson et al.
patent: 4856882 (1989-08-01), Oshima et al.

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