Integrated magnetically suspended control moment gyroscope control platform

A technology for controlling moment gyroscopes and control platforms, which is applied in the direction of aerospace vehicle guidance devices, etc., can solve problems such as inability to perform effective high-speed communication, insufficient CPU computing power, and inability to communicate at high speeds, etc., to improve computing speed and computing accuracy, computing Speed ​​and control accuracy are not high to avoid, improve the effect of flexibility and anti-interference ability

Inactive Publication Date: 2007-06-06
BEIHANG UNIV
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  • Summary
  • Abstract
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  • Claims
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AI Technical Summary

Problems solved by technology

Therefore, effective high-speed communication cannot be carried out between the controlled components, and if the controlled components are changed or added, a large change must be made to the corresponding hardware
In addition, from the perspective of economy, if the existing system wants to ensure high-precision control of each controlled component, it must use a relatively advanced CPU, and using a high-speed and highly integrated CPU to control only one component will cause a large resource consumption. waste
If a high-speed and highly integrated CPU is used to control multiple components, there is a problem that the computing power of the CPU is not enough
Therefore, the existing technology has the problems of inability to carry out effective high-speed communication between the controlled components, poor system flexibility and waste of resources.

Method used

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  • Integrated magnetically suspended control moment gyroscope control platform
  • Integrated magnetically suspended control moment gyroscope control platform
  • Integrated magnetically suspended control moment gyroscope control platform

Examples

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Embodiment Construction

[0017] As shown in Figure 1, the controlled components of the magnetic levitation control torque gyroscope adopted in this embodiment include a high-speed motor A, a high-speed motor B, a frame servo motor, a magnetic bearing A, a magnetic bearing B and a magnetic bearing Z. The present invention includes an application layer 1, a system layer 2, a field bus 3 and a control layer 4. The application layer 1 is built on the system layer 2, and the system layer 2 communicates with the control layer 4 through the field bus 3. The application layer 1 includes a state acquisition module 5, a monitoring module 6, a communication module 7 and a man-machine interface module 8, which mainly complete the sensor data acquisition, complex algorithm calculation and monitoring functions. The state acquisition module 5 collects the current, speed, and position of the high-speed motor A, the high-speed motor B, and the frame motor, as well as the current and position signals of the magnetic be...

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Abstract

The integrated magnetically suspended control moment gyroscope control platform for the integrated control of the magnetically suspended control moment gyroscope system includes mainly an application layer, a system layer, a field bus and a control layer. The application layer on the control layer completes the signal data acquisition, complicated algorithm calculation and monitoring, and includes a state acquisition module, a monitoring module, a communication module and a man-machine interface module. The system layer providing the application layer with operation platform and real-time datum includes an application platform based on CORBA protocol, a RTOS and an embedded hardware system. The control layer completes the control on the current loop of the controlled parts, including FPGA motion control card based on Nios II, high speed motor, frame motor, etc. The system layer communicates with the control layer through the field bus.

Description

technical field [0001] The invention relates to an integrated magnetic levitation control moment gyro control platform, which is mainly used in attitude control systems in the field of aerospace. Background technique [0002] The control moment gyroscope is an important attitude control actuator on large spacecraft and space stations. Compared with the traditional mechanical control moment gyroscope, the magnetic levitation control moment gyroscope has the advantages of large torque output and low vibration, so it has a wide range of high-precision large satellites and space stations. application prospects. [0003] The existing magnetic levitation control torque gyroscope servo system is centralized control according to different components, such as a set of controllers for high-speed motors, a set of control systems for frame servo motors, and a set of control systems for magnetic bearings. Therefore, effective high-speed communication cannot be carried out between the co...

Claims

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Application Information

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IPC IPC(8): B64G1/28
Inventor 房建成李海涛于灵慧王宗省贾军
Owner BEIHANG UNIV
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