Full-closed-loop interference rate compensation self-stabilization control method under geodetic coordinate system

A geodetic coordinate system and control method technology, applied in the field of artillery stability control system, can solve problems such as shock vibration, affecting stability, and insufficient stiffness

Active Publication Date: 2021-04-23
西北机电工程研究所
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Problems solved by technology

However, it was found in the project that the traditional suppressed artillery has undergone certain adaptation and improvement to achieve self-stabilization of the artillery at a large firing angle. The barrel-pointed strapdown inertial navigation is used as the stability of the position full-closed loop control system, causing small error jitter, and the backlash "shock vibration" phenomenon is obvious
The turret rate and the vehicle body rate are estimated by the g

Method used

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  • Full-closed-loop interference rate compensation self-stabilization control method under geodetic coordinate system
  • Full-closed-loop interference rate compensation self-stabilization control method under geodetic coordinate system
  • Full-closed-loop interference rate compensation self-stabilization control method under geodetic coordinate system

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[0090]The invention is further illustrated in connection with the accompanying drawings and examples, and the present invention includes, but is not limited to the following examples.

[0091]The invention includes the following steps:

[0092](1) Start control, set the number of control steps to J, I, and:

[0093]J = J + 1

[0094]Where J is the number of speed rings control steps in the stable system, the control cycle Ts= 1ms; i is the number of control steps of the stable system position ring, the control period T = 10ms, J is 10 times faster; J and I initial value are 0;

[0095](2) Judgment J% 10 = 0? Yes, i = i + 1, and transfer to step (3); otherwise transfer (9) step;

[0096](3) Collect SINS's aeroise ψ (i), θ (i),Wherein (i) is the navigation angle of SINS; θ (i) is the pitch angle of SINS;The horizontal rolling angle of sins;

[0097](4) Belt-resistant filters of the navigation angle and the pitch angle:

[0098]ψ '(i) = B10ψ (i) + b11ψ (i-1) + B12ψ (i-2) -a11ψ '(i-1) -a12ψ '(i-1)

[0099]θ '(i) ...

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Abstract

The invention provides a full-closed-loop interference rate compensation self-stabilization control method under a geodetic coordinate system. The full-closed-loop interference rate compensation self-stabilization control method comprises the steps that a course angle, a pitch angle and a roll angle of an SINS are gathered, and a high-low angle and an azimuth angle of an artillery are gathered; angular velocity values of an SINS gyroscope group, a turret gyroscope group and a vehicle body gyroscope are gathered, interference angular rates in an azimuth direction and a high-low direction under the geodetic coordinate system are extracted, and filtering correction is performed to obtain azimuth and high-low compensation angular rate control quantities; the stable control rate control instruction and the interference compensation angular rate control instruction are combined to serve as a servo drive speed total instruction; and high-low and azimuth servo drivers gather respective motor angular rates, perform high-order sliding mode speed control strategy calculation according to the speed control instruction to obtain a current loop control instruction and drive motors to control artillery turning motions according to a given control quantity. The full-closed-loop interference rate compensation self-stabilization control method under the geodetic coordinate system has the advantages of being high in response bandwidth, accurate in interference rate compensation and the like, and the artillery barrel pointing high-precision stability under the condition of a movable base seat large firing angle is realized.

Description

technical field [0001] The invention belongs to the field of artillery stabilization control systems, and mainly relates to an accurate and stable artillery follow-up system control method under a high dynamic dynamic base. Background technique [0002] With the development and evolution of military struggles, new military operational requirements urgently require suppression weapons to have the ability to shoot on the move, and self-propelled artillery is required to be able to perform combat tasks of action vs. static and dynamic vs. action. Then the artillery needs to be under the control of the aiming stabilization system to overcome the disturbance caused by the vehicle body due to the walking road and keep the artillery pointing stable. Such functions have already been realized in the gun control systems of tank weapons or amphibious assault guns. [0003] The patent "Control Method of Gun Aiming Stabilization System Using Strapdown Inertial Navigation" is applied to ...

Claims

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Application Information

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IPC IPC(8): F41G5/00F41G5/26
CPCF41G5/00F41G5/26
Inventor 李伟任海波韩磊位红军马捷
Owner 西北机电工程研究所
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