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Gravity-assisted strapdown inertial navigation method based on bayesian recursion filtering

A strapdown inertial navigation and recursive filtering technology, applied in navigation, surveying and navigation, navigation calculation tools, etc., can solve the problems of destroying the concealment of the strapdown inertial navigation system, the radio positioning method being easily interfered, and being unable to be used normally.

Active Publication Date: 2014-07-02
HARBIN ENG UNIV
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Problems solved by technology

However, when other traditional navigation methods such as GPS are used to correct the strapdown inertial navigation system, the concealment of the strapdown inertial navigation system will be destroyed, and radio positioning methods such as GPS are easily interfered, and even deceived by the enemy using technical means, making it cannot be used properly, so the strapdown inertial navigation system must be corrected by other passive methods of navigation

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  • Gravity-assisted strapdown inertial navigation method based on bayesian recursion filtering
  • Gravity-assisted strapdown inertial navigation method based on bayesian recursion filtering
  • Gravity-assisted strapdown inertial navigation method based on bayesian recursion filtering

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Embodiment Construction

[0022] The present invention will be described in detail below with reference to the drawings and embodiments.

[0023] Basic block diagram of the principle of the system figure 1 It can be seen that the strapdown inertial navigation system uses the output of the gyroscope and accelerometer to perform strapdown inertial navigation calculations, and calculates the attitude information, speed information and position information of the ship at the current time. Then use the position information and speed information calculated by the strapdown inertial navigation system to perform Bayesian recursive filtering to estimate the optimal position error at the current moment. After obtaining the optimal position error estimate, use it to correct the strapdown inertial navigation system In order to obtain the optimal position information of the ship and improve the accuracy of the system, the algorithm flow chart of the system is as follows figure 2 As shown, the specific implementation...

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Abstract

The invention provides a gravity-assisted strapdown inertial navigation method based on bayesian recursion filtering. In a strapdown inertial navigation system, under the condition without correction, the error in longitude of the strapdown inertial navigation system is diverged along with the time. In order to inhibit divergency of the error of the system and under the premise without damaging the concealment of the strapdown inertial navigation system, the invention provides the gravity-assisted strapdown inertial navigation method based on the bayesian recursion filtering. The gravity-assisted strapdown inertial navigation method provided by the invention has the advantages that after the measurement information is obtained, the posterior probability density of a state variable is gained by utilizing the bayesian law from the prior probability of the state variable, so that a globally optimal solution of the state variable is obtained; and after being gained, the globally optimal solution of the state variable is utilized for correcting the position error of the strapdown inertial navigation system, so that the purpose of improving the positioning accuracy of the system is achieved.

Description

Technical field [0001] The invention relates to a strapdown inertial navigation system navigation method, in particular to a new gravity assisted strapdown inertial navigation method. Background technique [0002] Inertial navigation is an autonomous navigation method that uses inertial sensors, reference directions and initial positions to determine the attitude, position and speed of the carrier. It is not affected by the environment, carrier maneuvering and radio interference, can continuously provide all navigation parameters, has high relative accuracy in a short time, and is the most important autonomous navigation method. The fatal flaw of the inertial navigation system is that the gyro keeps drifting with time, and the navigation positioning error continues to accumulate with the navigation time. It must be recalibrated regularly by other positioning means such as GPS. However, when GPS and other traditional navigation methods are used to modify the strapdown inertial na...

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Application Information

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IPC IPC(8): G01C21/16
CPCG01C21/165G01C21/20
Inventor 奔粤阳杨晓龙阮双双夏健钟李敬春赵维珩刘适李明宇尹冬寒杨祥龙
Owner HARBIN ENG UNIV
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