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Dynamic adaptability matching method for precision and inertia satellite deep combination system of inertia device

A technology of inertial devices and system dynamics, applied in the field of navigation, can solve the problems of inertial device selection, physical performance testing of difficult prototypes, complex loop-assisted design and hardware implementation, etc., to achieve reliable principles, flexible means, and strong engineering reference. Effect with applied value

Inactive Publication Date: 2017-12-01
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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Problems solved by technology

However, since the deep combination system involves two systems of inertial navigation and satellite navigation, the complex loop-aided design and hardware implementation are the technical bottlenecks restricting its large-scale promotion and use.
[0003] Domestic and foreign scientific research institutions and researchers have done a lot of related work around the realization of the principle of deep combination and system development. However, in the process of system design, they often face the problem of inertial device selection under specified dynamic conditions. Due to the constraints of the test environment , it is difficult to directly use the prototype for physical performance testing, how to take dynamic adaptability into consideration in the design process is a very important issue
So far, there has been no report on a universal matching method between the precision of inertial devices and the dynamic adaptability of deep integrated systems of inertial satellites

Method used

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  • Dynamic adaptability matching method for precision and inertia satellite deep combination system of inertia device
  • Dynamic adaptability matching method for precision and inertia satellite deep combination system of inertia device
  • Dynamic adaptability matching method for precision and inertia satellite deep combination system of inertia device

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Embodiment Construction

[0038] The technical solutions of the present invention will be described in detail below in conjunction with the accompanying drawings.

[0039] The present invention designs a matching method between the precision of inertial devices and the dynamic adaptability of the deep integrated system of inertial satellites, uses mathematical derivation to obtain the propagation characteristics of errors of inertial devices, and calculates the receiver parameter configuration, the error level of inertial devices and the The steady-state tracking error of the loop under dynamic conditions can be used to judge the stability of the loop, which solves the problem of device selection and parameter configuration selection for deep combination systems in high dynamic scenarios. The flow chart of the method is shown in figure 1 shown. The specific process is as follows.

[0040] Step 1. Establish an inertial device error model including g-sensitive errors in a high dynamic environment:

[0...

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Abstract

The invention discloses a dynamic adaptability matching method for the precision and inertia satellite deep combination system of an inertia device and belongs to the technical field of navigation. The method is used for solving the choose type problem for the inertial device during the practical application process of the inertial / satellite deep combination system. Through analyzing the influence situation of the dynamic environment of a carrier on the inertia device, the propagation characteristics of the error of the inertial device is deduced. Meanwhile, the parameter configuration of a current receiver, the error grade of the inertial device and the loop steady-state tracking error of the carrier in the dynamic state are calculated. As a result, the loop stability is judged. Finally, the device selection and the parameter configuration of the deep-combination practical system under the high-dynamic scene are finally realized. According to the method of the invention, the device selection and system parameter configuration work under specified dynamic indexes can be effectively guided. Therefore, the method has strong engineering reference and application value.

Description

technical field [0001] The invention belongs to the technical field of navigation, and in particular relates to a method for matching the precision of an inertial device and the dynamic adaptability of an inertial satellite deep combination system. Background technique [0002] The inertial / satellite integrated navigation system is a mainstream navigation method in the field of navigation at present, and the deep integrated navigation technology introduces the inertial information into the receiver loop, so that the system has both high precision and high dynamic stability. Research frontiers in the field of navigation. However, since the deep combination system involves two systems of inertial navigation and satellite navigation, the complex loop aided design and hardware implementation are the technical bottlenecks restricting its large-scale promotion and use. [0003] Domestic and foreign scientific research institutions and researchers have done a lot of related work a...

Claims

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Application Information

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IPC IPC(8): G01S19/47G01C21/16G01C21/18G01C21/00G06F17/11
CPCG01C21/005G01C21/165G01C21/18G01S19/47G06F17/11
Inventor 陈驵赖际舟李荣冰刘建业季国田赵宏宇
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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