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An Estimation Method of Projectile Roll Angle Based on GPS and Least Square Filter

A least squares, roll angle technology, applied in the field of navigation, can solve the problem that the roll angle estimation is not easy to obtain accurately, and achieve the effect of high precision

Active Publication Date: 2021-11-02
SOUTHEAST UNIV
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  • Application Information

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Problems solved by technology

Moreover, the air is easily affected by wind and other meteorological environments, and the estimation of the roll angle is not easy to obtain accurately. Therefore, correcting the roll angle of guided projectiles is a hot topic of research at home and abroad.

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  • An Estimation Method of Projectile Roll Angle Based on GPS and Least Square Filter
  • An Estimation Method of Projectile Roll Angle Based on GPS and Least Square Filter
  • An Estimation Method of Projectile Roll Angle Based on GPS and Least Square Filter

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Embodiment Construction

[0049] The technical solutions of the present invention will be described in detail below, but the protection scope of the present invention is not limited to the embodiments.

[0050] The present invention is applicable to the estimation of the roll angle when the projectile is in flight, first define the following coordinate system:

[0051] Navigation system n: the origin is where the shell is located, the Y axis points to the geographic north, the X axis points to the geographic east, and the Z axis is perpendicular to the ground level and points upward.

[0052] Carrier system b: the origin is the center of mass of the projectile, the Y axis moves forward along the forward direction of the projectile, the X axis points to the right, and the Z axis points upward.

[0053] Navigation inertial frame i n : The navigation system n at the initial moment is solidified in the inertial space and does not change with time.

[0054] Carrier inertial frame i b : The carrier body b...

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Abstract

The invention discloses a method for estimating the roll angle of a projectile based on GPS and least squares filtering. The method includes the following steps: (1) Calculate the inertial frame i of the carrier at time t according to the velocity and position of the projectile provided by the gyroscope and GPS b system is relative to the shell attitude matrix of the carrier system b, the navigation system n is relative to the navigation inertial system i n The shell attitude matrix (2) calculates the shell in the carrier inertial frame i b and navigation inertial frame i n The speed value under the system and (3) the speed ratio provided by GPS to calculate the initial heading angle Y 0 and pitch angle P 0 , set the state variable X according to the initial roll angle; (4) estimate X according to the least squares filter and calculate it as i n system relative to i b (5) Calculate the roll angle of the shell according to the sum at time t; where is the attitude matrix of the n system relative to the b system at the time t.

Description

technical field [0001] The invention belongs to the technical field of navigation, in particular to a method for estimating the roll angle of a shell based on GPS and least square filtering. Background technique [0002] A guided projectile is a low-cost, miniaturized precision-guided weapon, generally equipped with a GPS / INS combination. In the precise control flight technology of ammunition, the real-time and accurate measurement of the roll angle is the basis for the implementation of guidance or correction control, and it is also the key to the long-range and precise flight of the guided munition. In such a severe situation, the IMU cannot be powered on normally in this high overload shock environment, and the initialization of the navigation system needs to be completed autonomously in the air after launch. Moreover, the air is easily affected by wind and other meteorological environments, and it is difficult to estimate the roll angle accurately. Therefore, correcting...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01C21/16G01C21/20G01S19/47
CPCG01C21/165G01C21/20G01S19/47
Inventor 刘锡祥杨文强许广富马晓爽郭小乐
Owner SOUTHEAST UNIV
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