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SoC chip structure applied to gyroscope control system

A technology of control system and chip structure, which is applied in the direction of general control system, control/regulation system, program control, etc., can solve the problems of large volume and high complexity of discrete device solution development, and achieve the effect of low single chip

Pending Publication Date: 2021-06-15
AEROSPACE SCI & IND MICROELECTRONICS SYST INST CO LTD
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  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0003] The purpose of the present invention is to overcome the deficiencies in the prior art, provide a SoC chip structure applied to the gyro control system, realize the monolithic and low power consumption of the gyro control and processing system, and solve the problem of the discrete components of the gyro control and processing system Problems with high complexity and large volume in solution development

Method used

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  • SoC chip structure applied to gyroscope control system
  • SoC chip structure applied to gyroscope control system

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Embodiment Construction

[0020] All features disclosed in all embodiments in this specification, or steps in all implicitly disclosed methods or processes, except for mutually exclusive features and / or steps, can be combined and / or extended and replaced in any way.

[0021] like figure 1 , as shown in 2, a SoC chip structure applied to the gyro control system, including bus, bridge, CPU subsystem, memory subsystem, control output subsystem, input sampling subsystem, peripheral subsystem and clock reset subsystem, The bus includes a high-speed bus and a low-speed bus; the high-speed bus is connected to the low-speed bus through a bridge; the CPU subsystem is connected to the high-speed bus, and the high-speed bus is connected to the memory subsystem and the bridge respectively; the control output subsystem is connected to the low-speed bus , the low-speed bus is connected to the bridge; the input sampling subsystem is connected to the low-speed bus; the peripheral subsystem is connected to the low-spee...

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Abstract

The invention discloses an SoC chip structure applied to a gyroscope control system. The SoC chip structure comprises buses, a bridge, a CPU subsystem, a memory subsystem, a control output subsystem, an input sampling subsystem, a peripheral subsystem and a clock reset subsystem; the buses comprise a high-speed bus and a low-speed bus; and the high-speed bus is connected with the low-speed bus through the bridge. According to the SoC chip structure applied to the gyroscope control system, signals are output to a gyroscope braking subsystem through a DAC and a synchronous output module, signal conversion in the gyroscope control system is achieved through an ADC integrated in the chip, data analysis and processing are conducted through a 32-bit RISC CPU, and therefore loop control and the like of the gyroscope control system are achieved; and the problems of high system development complexity and large size of a discrete device integration implementation scheme of the gyroscope control system are effectively solved.

Description

technical field [0001] The invention relates to a SoC chip structure in the field of precision control, and more specifically, relates to a SoC chip structure applied to a gyroscope control system. Background technique [0002] At present, the control system of the gyro is mainly realized by discrete devices such as FPGA+ / ADC / DAC. For example, when domestic and foreign companies and related units are developing and designing gyro control systems, they adopt the solution of integrating discrete devices such as FPGA+ADC / DAC chips, such as figure 1 shown. This is mainly because there is currently no dedicated control SoC chip developed for the application requirements of the gyro control system, so only the secondary integration of discrete devices can be used, which increases the complexity of the development of the gyro system, and the control realized by the integration of discrete devices The size of the system is large, making the miniaturization of the gyroscope a bottl...

Claims

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Application Information

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IPC IPC(8): G05B19/042
CPCG05B19/0423G05B2219/24215
Inventor 武春风刘林涛白明顺秦勇莫尚军
Owner AEROSPACE SCI & IND MICROELECTRONICS SYST INST CO LTD
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