Integrating double-framework magnetically suspended control moment gyroscope (MSCMG) magnetic bearing control system

A technology for controlling torque gyroscopes and control systems, applied to bearings, shafts and bearings, and controlling mechanical energy, etc., can solve problems such as online debugging and modification, and achieve the effect of simple and reliable connection, simplified work, and complete transmission

Inactive Publication Date: 2011-07-27
BEIHANG UNIV
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  • Abstract
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  • Claims
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AI Technical Summary

Problems solved by technology

The existing control system does not propose a complete set of solutions for online debugging and modification of parameters in the control process

Method used

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  • Integrating double-framework magnetically suspended control moment gyroscope (MSCMG) magnetic bearing control system
  • Integrating double-framework magnetically suspended control moment gyroscope (MSCMG) magnetic bearing control system
  • Integrating double-framework magnetically suspended control moment gyroscope (MSCMG) magnetic bearing control system

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Embodiment Construction

[0044] like figure 1 As shown, the integrated dual-frame magnetic suspension control moment gyro magnetic bearing control system of the present invention is composed of a control circuit 3, an acquisition circuit 4 and a communication interface 2, wherein the control circuit 3 includes a DSP module 31, an FPGA module 32, Flash33, SRAM34, Speed ​​measurement module 35; Acquisition circuit 4 includes D / A module 41, A / D module 42 and double-frame speed / position interface circuit 43, displacement sensor interface circuit 44, current sensor interface circuit 45; Communication interface 2 includes USB interface 21, RS232 and SPI interface 23:

[0045] The FPGA module 32 controls the A / D module 42 to receive the current value, displacement value, rotational speed and position value of the inner and outer frames at a sampling frequency of 7 kHz. The maximum value of the displacement voltage signal transmitted by the displacement sensor 11 is 6V, the minimum value is 4V, and the volt...

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Abstract

The invention is an integrating double-framework magnetically suspended control moment gyroscope (MSCMG) magnetic bearing control system, comprising a control circuit, a collecting circuit and a communication interface; wherein, the control circuit comprises a FPGA module, a DSP module and the like; the collecting circuit consists of current, a displacement sensor interface circuit, a double-framework revolution / position interface circuit, an A / D module, and a D / A module; the communication interface comprises a USB interface, RS232 and an SPI interface; the control circuit in the system is used for receiving gyroscope rotor signal processed by the collecting circuit, controlling the stable suspension thereof, transmitting the controlled variable to an upper computer through the communication interface, and realizing on-line monitoring on the suspended gyroscope rotor, data collecting and on-line modification for the controlled variable under the control of the upper computer. The system provided in the invention has the advantages of effectively communicating an inner framework and an outer framework rotational signals under the control of high precision, realizing the integratingdesign of the control system and the measurement and control system, and satisfying the requirements of speed and precision for the data collecting and the on-line monitoring.

Description

technical field [0001] An integrated double-frame magnetic suspension control moment gyro magnetic bearing control system, which is used for high-precision suspension control of the double-frame magnetic suspension control moment gyro rotor, can realize fast and non-interference signal transmission with the frame control system, and control parameters For high-speed data acquisition and online monitoring, and online modification of key variable values, it is suitable for high-precision, highly integrated servo mechanism control systems. Background technique [0002] Control Moment Gyroscope (CMG) is a kind of actuator used for spacecraft attitude control. Compared with traditional attitude control mechanisms such as jet thrusters and momentum wheels, the control moment gyroscope has significant advantages such as large control range, high precision, large output torque, and only needs electric energy to work, so it is used in large spacecraft such as space stations. Double ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H02K7/09H02N15/00F16C32/04
Inventor 房建成王英广丁力郑世强陈冬王灿
Owner BEIHANG UNIV
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