Frequency domain solution time delay fuzzy method for deep space antenna

An antenna array, frequency domain technology, applied in the field of deep space antenna array frequency domain time delay ambiguity resolution, can solve the problems of time delay ambiguity, influence delay accurate correction, different transmission paths, etc., to get rid of transition dependence, guarantee The effect of precision

Active Publication Date: 2015-11-11
10TH RES INST OF CETC +1
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Problems solved by technology

The main problem in the deep space downlink antenna array is that the signal arrives at each unit antenna in the antenna array and the transmission path between each unit antenna and the signal combiner is different, resulting in a time-varying delay difference when the signal reaches the combiner
The correction of the time delay difference in the existing antenna array synthesizer is based on the pre-correction table generated by prior information such as the station site and the trajectory of the spacecraft. Usually, the accuracy of the pre-correction table is too low, which will cause the delay to be blurred and affect the time delay. Delayed Accurate Correction

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  • Frequency domain solution time delay fuzzy method for deep space antenna

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Embodiment Construction

[0010] refer to figure 1 . exist figure 1 In the described process of solving delay ambiguity in the frequency domain: according to the approximate geometric orientation between the spacecraft and the ground station, the initial delay range between the receiving channels of the antenna array is given, and the phase spectrum in the frequency domain is calculated according to the initial delay. Fuzzy frequency range; then obtain a precise estimate of the time delay by curve fitting within this range, and correct the time delay between channels according to the estimated result; according to the correction accuracy of the time delay, obtain the frequency at which the phase spectrum in the frequency domain is not ambiguous range, and then obtain a further fine estimate of the time delay through curve fitting within this range, and correct the time delay between channels according to the estimated result; if the time delay correction accuracy meets the requirements, exit, otherwis...

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Abstract

The invention proposes a frequency domain solution time delay fuzzy method for a deep space antenna and aims at providing the method which does not depend on prior information (accurate site location and the transit trajectory of a spacecraft). The method is achieved through the following technical scheme which comprises the steps: calculating and obtaining a non-fuzzy frequency range of a frequency domain phase spectrum in an initial time delay range between given channels according to the geometric orientation between the spacecraft and a ground station; carrying out the correction of time delay between channels in the range according to the precise estimation results, obtained through curve fitting, of time delay; updating the non-fuzzy frequency range of the frequency domain phase spectrum according to the correction precision of time delay, obtaining the further precise estimation of time delay in the range through curve fitting, and carrying out the correction of time delay between channels according to the estimation results; carry out quitting if the correction precision of time delay meets the requirements, or else repeating the last step till the correction precision of time delay meets the requirements. The method gets rid of the excessive dependence on accurate site location and the transit trajectory of the spacecraft.

Description

technical field [0001] The invention relates to a method for solving time-delay ambiguity in the frequency domain of a deep-space antenna array. Background technique [0002] The challenges faced by deep space measurement and control communication are: longer distance, higher data rate, and more robust emergency measurement and control communication. Typical technical approaches to improve system transmission capabilities include: building larger-diameter antennas, developing receivers with lower noise, using newer encoding and decoding schemes, and so on. The cost of these technical approaches is extremely high, and the performance of the overall system can only be gradually improved a little bit. Using a large number of small antenna arrays to achieve the performance of large antennas with the same equivalent aperture and reducing maintenance costs is the key development direction of subsequent deep space measurement and control communications. The main problem in the de...

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Application Information

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IPC IPC(8): H04B7/04H04B7/08H04W56/00
CPCH04B7/04H04B7/0894H04W56/0035H04W56/005
Inventor 徐茂格赵卫东冯林高
Owner 10TH RES INST OF CETC
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