Digital control system for satellite aerial directing mechanism

A digital control system and pointing mechanism technology, applied in the direction of electrical program control, comprehensive factory control, etc., can solve the problems that the position detection sensor and controller cannot be integrated, it is difficult to meet the development requirements of the mechanism control system, and the operation rate of the single-chip computer is low. , to achieve the effect of reducing system switching loss, reducing the number of chips and the scale of the circuit, and improving the integration level

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

Problems solved by technology

At present, the existing control system is based on single-chip microcomputer, but due to the low operation rate and small number of calculation bits of single-chip microcomputer, the functions that can be realized are very limited, and it is more and more difficult to meet the development requirements of the future pointing mechanism control system.
However, the digital control system based on DSP+FPGA, because of the addition of control chips, configuration chips and a large number of memory chips, the reliability of the system is reduced and the power consumption of the system is also increased.
Single-chip FPGA is generally suitable for the construction of control logic, but its computing power is very limited, making it difficult to realize complex operations
Moreover, the existing digital controller can only be used as a motor-driven controller, and also requires a special position detection module and chip, and cannot achieve the integration of position detection sensors and controllers.

Method used

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  • Digital control system for satellite aerial directing mechanism
  • Digital control system for satellite aerial directing mechanism
  • Digital control system for satellite aerial directing mechanism

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Embodiment Construction

[0022] like figure 1 As shown, the present invention adopts an on-board 28V power supply 11 to supply power, and the on-board 28V power supply 11 obtains the +3.3V and +1.9V power supplies and The +5V, +12V, ±5V, ±12V power supplies required by the communication module 15, the excitation module 9, and the decoding module 10; the protection circuit 1 is connected to the secondary power supply module 2 to prevent excessive current and protect the circuit; the secondary The power supply module 2 is connected with the power conversion chip 12 of the power module 3, and is used to supply power to the power module 3 and the DSP controller 14 respectively; the PWM excitation signal output from the DSP controller 14 is sent into the rotary transformer 6 through the excitation module 9, and is transferred from the rotary transformer The stimulated signal output by the transformer 6 is returned to the DSP controller 14 through the decoding module 10 to complete the calculation of the ou...

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Abstract

The invention discloses a digital control system for a satellite aerial directing mechanism which is applied to driving and controlling a novel high-precision reliable satellite aerial directing mechanism. The system comprises a digital signal processor (DSP), a synchronous machine, a rotary transformer, a Hall effect rotor position sensor, an exciting output circuit, an axial angle decoder circuit, a three-phase bridge type power module, a PWM driving circuit, a three-phase winding current detecting circuit, a communication module circuit, a secondary power supply transfer circuit, and a protection circuit. The system can realize the high-precision control for the satellite aerial directing mechanism by the upper computer communication, the output shaft position detection, the winding current detection, the motor rotor position detection and a series of control methods.

Description

technical field [0001] The invention relates to a digital control system of a satellite antenna pointing mechanism. The system has the advantages of high integration, small volume, low power consumption and high reliability, and is suitable for high-precision pointing control of satellite antennas. Background technique [0002] The pointing mechanism is the motion actuator of the satellite antenna, which plays an important role in the whole star system. At present, with the development of my country's large-scale communication satellite and relay satellite technology, higher requirements are put forward for the accuracy, life and reliability of the digital control system of the satellite antenna pointing mechanism. Therefore, it is imminent to design a digital control system for pointing mechanism with high precision, high integration and high reliability. Many domestic units have carried out many beneficial explorations on the development of pointing mechanism technology, ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05B19/418
Inventor 刘刚刘强李光军王志强姜迪开
Owner BEIHANG UNIV
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