Strapdown inertial/satellite integrated navigation detecting system and simulation testing method thereof

A technology of integrated navigation and strapdown inertial navigation, which is applied in satellite radio beacon positioning system, radio wave measurement system, measuring device, etc., can solve the problems that have not yet been realized, and achieve real-time and accurate integrated navigation information, improve accuracy and Verification and evaluation of quality and the effect of strong versatility
CN103308073AActive Publication Date: 2013-09-18SHANGHAI JIAO TONG UNIV
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Patent Information

Authority / Receiving Office
CN · China
Current Assignee / Owner
SHANGHAI JIAO TONG UNIV
Publication Date
2013-09-18

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Abstract

The invention relates to a strapdown inertial / satellite integrated navigation detecting system and a simulation testing method thereof. The system comprises a strapdown inertial subsystem, a satellite navigation subsystem, a navigation module and a control and display module, wherein the control and display module is connected with the strapdown inertial subsystem and the satellite navigation subsystem respectively to transmit track information; the strapdown inertial subsystem and the satellite navigation subsystem are respectively connected with the navigation module to transmit angular speed, accelerated speed and satellite signals; the output end of the navigation module is connected with the control and display module to feed an integrated navigation result back to the control and display module to form a closed-loop system. The system has real error characteristics. According to the system, optional tracks can be generated and do not need to be carried by actual carriers, so that the research and development cycle of an integrated navigation system is shortened, and the research and development cost is reduced; the real-time dynamic simulation on carrier movement according to a preset track can be realized and finished, and the universality is very strong.
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Description

technical field

[0001] The present invention relates to a detection device and method in the technical field of satellite navigation, in particular to a strapdown inertial / satellite integrated navigation detection system and its simulation test method, which is applicable to the theoretical method and method of strapdown inertial / satellite integrated navigation system Research on engineering application technology, and performance analysis and verification of integrated navigation system. Background technique

[0002] Since the 1970s, the great achievements of modern control theory and the advancement of computer technology have provided a theoretical basis and technical support for the development of GNSS / INS integrated navigation technology and the development of navigation systems. In the past 40 years, integrated navigation technology has become one of the navigation technologies with the most application and development potential. Strapdown inertial / satellite integrated...

Claims

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