Navigating and steady aiming method of navigation / steady aiming integrated system

A stable pointing and platform technology, applied in the field of inertial navigation, can solve the problems of unsuitable inertial navigation system, difficulty in attitude alignment accuracy and alignment speed, and low accuracy

Inactive Publication Date: 2009-04-22
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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Problems solved by technology

[0005] In view of the potential requirements of combat vehicle equipment in the future combat environment, there is a strong demand for the comprehensive application of information perception and fire control and stabilization. Among the equipped systems, the two systems of steady sight and navigation can only be used in time-sharing, that is, steady sight and navigation cannot work at the same time, and the accuracy is not high
In China, there are relevant technical researches on the integrated system of aiming/north seeking, but this system can only solve the heading of the vehicle body, and cannot provide all-round attitude information, speed, and position information, that is, it cannot perform complete navigation work
[0006] The inertial navigation system is generally initialized under a static base. During the initialization process, the accuracy and alignment speed of the att

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  • Navigating and steady aiming method of navigation / steady aiming integrated system
  • Navigating and steady aiming method of navigation / steady aiming integrated system
  • Navigating and steady aiming method of navigation / steady aiming integrated system

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Embodiment Construction

[0021] In the traditional vehicle-mounted integrated system, it may not be able to provide all-round attitude information, speed, and position information, or the navigation system and the stabilization system cannot work at the same time. The present invention improves on the basis of the traditional integrated system, such as figure 1 As shown, the inertial measurement unit (IMU) is installed on the photoelectric stabilized aiming platform with random rotation. The IMU is composed of three orthogonally installed fiber optic gyroscopes and three orthogonally installed accelerometers. The stabilized aiming platform has For the rotation function, the gyro signal in the IMU is output to the platform stabilization circuit to realize the function of stabilizing the platform. At the same time, the signals of the gyroscope and accelerometer in the IMU are output to the inertial navigation calculation part to calculate the attitude, speed and position information of the stable aiming...

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Abstract

The invention relates to a navigating and stabilized sighting method of a navigation/stabilized sight all-in-one system, belonging to the inertial guidance field. The navigating method realizes stance and positioning on a load by an inertial measuring unit which is arranged on an electro-optical stabilized sighting platform. The method comprises the steps as follows: collecting the signal of the inertial measuring unit; fast and accurately initial aligning below the stabilized sighting platform; an inertial navigation algorithm based on vehicle-bone stabilized sighting platform; resolving heading attitude and analyzing the error thereof; analyzing the error of an inertial guidance system and an inertial part, modeling and compensating; and inertial guidance/milemeter/GPS multi-information fault-tolerance combined navigation. The navigation method overcomes the defects in the prior art that stabilized sighting and the navigation system can not work simultaneously and the all-in-one system can not provide full navigation information, can provide real-time, accurate and complete navigation heading attitude information and navigation positioning information for carriers (like a chariot), and can improve the battlefield viability and the comprehensive hosting ability.

Description

technical field [0001] The invention relates to a navigation positioning and attitude fixing method applied to a chariot navigation / sight stabilization integrated system, and belongs to the field of inertial navigation. Background technique [0002] Line-of-sight stabilization system and inertial navigation system are two high-precision inertial systems widely used in ground combat vehicles such as tanks in recent years. The main component of the line-of-sight stabilization system is the photoelectric stabilization platform, through which the line-of-sight is stabilized to provide accurate shooting or guidance references for the chariot while it is moving, which enhances the maneuverability of the chariot; the inertial navigation system can provide timely information on carrier attitude, The speed and location guide the tank to covertly enter the battlefield and strike the target. Its autonomy is unmatched by other positioning and orientation systems. [0003] The main comp...

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Application Information

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IPC IPC(8): G01C21/16G01C21/18
Inventor 钱伟行刘建业赵伟李荣冰赖际舟祝燕华赵文芳
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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