Design method of IMU digital filter for inertial navigation system

An inertial navigation system and digital filtering technology, applied in the IMU data processing field of the inertial navigation system, can solve the problems of simulation model establishment without knowledge reserve, simulation model and realization of code non-homology, manpower consumption, etc.

Inactive Publication Date: 2015-06-10
FLIGHT AUTOMATIC CONTROL RES INST
View PDF4 Cites 3 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The disadvantage of this design method is that there is no knowledge reserve in the establishment of the simulation model, and the non-homology between the simulation model and the implementation code will often cause repeated iterations of design, simulation, and implementation.
[0004] At present, the IMU special filter design, simulation and software implementation of the inertial navigation system are in a disconnected state, and the design results have no knowledge reserves, and it is entirely dependent on manpower to ensure the consistency of software implementation and design, which often brings about a large gap from design to implementation. Loop iteration is time-consuming and manpower-consuming, and the IMU special filter design of the inertial navigation system has no previous experience and knowledge for reference, the development efficiency is low, and the reliability and safety are poor

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Design method of IMU digital filter for inertial navigation system
  • Design method of IMU digital filter for inertial navigation system
  • Design method of IMU digital filter for inertial navigation system

Examples

Experimental program
Comparison scheme
Effect test

Embodiment

[0030] The following describes the design process of a digital filter dedicated to a certain type of IMU in conjunction with the attached drawings:

[0031] 1. According to the low-pass digital filtering algorithm and data processing characteristics used in the IMU special digital filter of the inertial navigation system, the modeling design method is used to establish such figure 2 The IMU-specific digital filter component model library shown. It includes data transposition, data shift, data multiplication, data comparison, input data detection and other data processing component models, and a special digital filtering algorithm model (low_fliter_cpu1) for the IMU of the inertial navigation system; the model algorithm is this The output value of the secondary filter is equal to the sum of multiplying the latest N+1 sets of data by the B0~Bn parameters, and then subtracting the sum of the multiplication of the output values ​​of the previous N beats by the A1~An parameters. ...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

PUM

No PUM Login to view more

Abstract

The invention relates to a design method of an IMU (inertial measurement unit) digital filter for an inertial navigation system. The adopted the scheme is that the design method comprises the following steps: through overall planning, dividing an IMU special filter for the inertial navigation system into various filter assemblies by class, extracting parameters of each assembly, designing and establishing various filter assembly models to form an IMU special digital filter assembly model library, reestablishing a combination and reconfiguring parameters according to different IMU needs by selecting the assemblies from the IMU special digital filter assembly model library to form a filter model meeting IMU special data processing needs of different inertial navigation systems, determining the filter model through data simulation verification of the models, and automatically converting the model into an embedded system code. By the design method, quick and efficient design of the IMU special filter of the inertial navigation system is achieved; the IMU special filter has good certainty, simulation, testability and extensibility; the consistency of design, simulation and achievement is effectively ensured.

Description

technical field [0001] The invention belongs to the field of IMU (inertial measurement unit) data processing of an inertial navigation system, and relates to an IMU digital filter design method for an inertial navigation system. Background technique [0002] IMU is an inertial measurement component commonly used in inertial navigation systems. Its data processing depends on different IMUs and the inertial systems loaded by the IMU. The signal processing filters for sampling inertial components have different requirements in terms of algorithm structure and parameter configuration. In the construction of the IMU digital signal processing filter of the inertial navigation system, it is necessary to design, simulate and verify separately for various types of IMUs and the inertial navigation systems loaded there. [0003] The construction method of the IMU digital signal processing filter of the original inertial navigation system is as follows: first, according to the character...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

Application Information

Patent Timeline
no application Login to view more
Patent Type & Authority Applications(China)
IPC IPC(8): G06F17/50
Inventor 杨黎徐晓乐张向虎姚志强
Owner FLIGHT AUTOMATIC CONTROL RES INST
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products