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A Vibration Suppression Method Based on Stewart Active Platform

Active Publication Date: 2017-06-16
HUAZHONG UNIV OF SCI & TECH
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  • Description
  • Claims
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AI Technical Summary

Problems solved by technology

[0003] Compared with passive theory, active vibration isolation produces significant performance enhancements, but it requires sensors, actuators, algorithm processors, which requires active vibration isolation to be reliable and efficient in terms of load and power consumption
Although pure active feedback control can effectively solve the first inherent contradiction of vibration isolation performance, the active algorithm is still not efficient enough to solve the second contradiction in the vibration isolation system, and cannot meet the precise vibration isolation requirements of satellite platforms

Method used

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  • A Vibration Suppression Method Based on Stewart Active Platform
  • A Vibration Suppression Method Based on Stewart Active Platform
  • A Vibration Suppression Method Based on Stewart Active Platform

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Embodiment Construction

[0062] In order to make the objectives, technical solutions, and advantages of the present invention clearer, the following further describes the present invention in detail with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, but not to limit the present invention. In addition, the technical features involved in the various embodiments of the present invention described below can be combined with each other as long as they do not conflict with each other.

[0063] figure 1 It is a micro-vibration suppression platform-piezoelectric Stewart vibration isolation platform structure configuration layout. The piezoelectric Stewart vibration isolation platform consists of load platform 7, basic platform 8, and piezoelectric single-leg structure (1#, 2#, 3# , 4#, 5#, 6#), the load platform 7 and the basic platform 8 pass through the piezoelectric single-leg struct...

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Abstract

The present invention discloses a Stewart active platform and a vibration abatement method. The Stewart active platform includes a load platform, a basic platform, a controller, an acceleration sensor and piezoelectric single-legged structures. Each piezoelectric single-legged structure includes an upper flexible hinge, a force sensor, a piezoelectric actuator, and a lower flexible hinge. The force sensor, the piezoelectric actuator and the acceleration sensor are connected to the controller. The method includes the steps as follows: 1) the controller acquires a feedback control signal; 2) the controller acquires a feedforward control signal; 3) the controller acquires a composite control voltage of a feedback voltage and a feedforward voltage; 4) and the composite control voltage is outputted to the piezoelectric actuator, and the piezoelectric actuator applies an acting force to the load platform. A control algorithm adopted by the invention, which utilizes a PI force feedback algorithm, not only can effectively reduce a natural system frequency and a vibration resonance peak, but also efficiently iterate by the utilization of an RLS adaptive algorithm with an efficient evaluation performance so as to find an optional weight value, and thereby reducing the vibration of the load platform.

Description

Technical field [0001] The invention belongs to the field of vibration control, and more specifically, relates to a Stewart active platform and a vibration suppression method based on the Stewart active platform. Background technique [0002] In the vibration system, passive vibration isolation presents a reliable, low-cost solution, which can effectively attenuate broadband high-frequency vibration isolation. However, due to two inherent contradictions in the vibration isolation system: the contradiction between the vibration attenuation capacity in the high and low frequency bands, the contradiction between the foundation vibration isolation ability and the ability to resist direct interference from the foundation, it cannot meet the isolation requirements of ultra-precision equipment. Vibration requirements, for example, a spacecraft flying in orbit is not in a free-drift state (weightless state), and various responses will cause disturbances similar to gravitational accelerat...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05D19/02
Inventor 陈学东王敏李小清陶业英明平光李明
Owner HUAZHONG UNIV OF SCI & TECH
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