Null widened interference suppression method of high-dynamic satellite navigation system

A technology for satellite navigation system and interference suppression, which is applied in the field of satellite navigation system interference suppression, can solve problems such as being unable to be suppressed, narrow null traps, and interference easily moving out of the direction pointed by null traps, so as to reduce the false capture rate and output signal The effect of dry ratio increase

Inactive Publication Date: 2011-05-04
CIVIL AVIATION UNIV OF CHINA
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Problems solved by technology

However, these methods can effectively suppress interference only when the receiver is in a static or low dynamic environment
When the receiver is in a highly dynamic environment, the performance of the algorithm will be seriously affected
This is because in a highly dynamic environment, the movement speed of the satellite navigation receiver carrier is generally greater than 1km / s. In war, the satellite navigation receiver carrier is often only tens or hundreds of kilometers away from the enemy jammer, causing interference relative to the satellite The direction of the navigation receiver changes quickly, and the null trap formed by the anti-jamming algorithm under low dynamics is too narrow, and the interference can easily move out of the direction pointed by the null trap and cannot be suppressed

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  • Null widened interference suppression method of high-dynamic satellite navigation system
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  • Null widened interference suppression method of high-dynamic satellite navigation system

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Embodiment Construction

[0028] The method for suppressing interference of a high dynamic satellite navigation system with widening nulls according to the present invention will be described in detail below in conjunction with the embodiments and accompanying drawings.

[0029] Since the carrier of the satellite navigation receiver is in a state of high-speed motion in a highly dynamic environment, even if the interference source is stationary, the direction of the interference relative to the satellite navigation receiver is constantly changing. When the distance between the interference source and the receiver is short, the speed of change of the interference relative to the direction of the receiver will be very fast. If the width of the null of the array antenna beam in the interference direction is very narrow, as the receiver moves, the null of the antenna beam is easily moved out of the interference direction, and the interference will not be suppressed, and the satellite navigation receiver wil...

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Abstract

The invention discloses a high dynamic satellite navigation system interference suppression method widening zero defect, the method comprises: respectively down-frequency conversing N ways of radio frequency signals received by the N (N>2) element aerial array into IF signals; respectively performing the A / D conversion for the IF signals in the N ways obtained by the down-frequency conversion; obtaining the orthogonal complement space of the interference subspace based on the relation between the interference power and the satellite signal and the noise power, by using the N ways IF digital signals obtained in the step 2; calculating the new orthogonal complement space of the subspace relating to the differentiation order, the array element position and the interference subspace based on the differential constraint principle; combining the new orthogonal complement space of the subspace and the power invert algorithm to calculate the weighting vector of the aerial array based on the wave packet zero defect width setting proportionality coefficient to be reached by using the obtained new orthogonal complement space of the subspace in the step4. The invention can enable the output signal inference ratio of the satellite navigation receiver under high dynamic environment to be obviously increased, and can reduce the mis-capturing rate of the satellite signal by the satellite navigation receiver under high dynamic environment.

Description

technical field [0001] The invention relates to a satellite navigation system interference suppression method. In particular, it relates to a high dynamic satellite navigation system interference suppression method for widening the null width of the antenna beam in the interference direction and widening the null. Background technique [0002] The satellite navigation system is composed of artificial satellites and ground support systems. It provides comprehensive real-time three-dimensional navigation and positioning services for sea, land, and air, and is widely used in civilian and military fields. In civilian use, the receiver carrier is in a static state or a low-dynamic motion state, while in military use, the speed, acceleration, and acceleration rate of the receiver carrier are often very large, which is called high dynamic. With the modernization of national defense, the requirements for the accuracy and reliability of flying object trajectory testing and flying ob...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01S1/04
Inventor 吴仁彪李婵卢丹
Owner CIVIL AVIATION UNIV OF CHINA
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