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Sea data processing realization method based on low-altitude sounding rocket

A sounding rocket and marine data technology, applied in the field of data processing, can solve problems affecting the processing results of marine data, imperfect quality control and processing methods, and limited application prospects, so as to achieve good data processing effects, improve accuracy and Credibility and the effect of improving data accuracy

Active Publication Date: 2018-10-23
TIANJIN UNIV
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AI Technical Summary

Problems solved by technology

However, at present, the quality control and processing methods of the data collected by low-altitude sounding rockets are not perfect, and the research on its scientific detection data and auxiliary engineering data still only stays in the overall system design, which affects the processing results and limit its application prospects

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  • Sea data processing realization method based on low-altitude sounding rocket
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  • Sea data processing realization method based on low-altitude sounding rocket

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Embodiment Construction

[0029] Step 1: Limit the range of data collected by the sounding rocket

[0030] The maximum ceiling of the sounding rocket is 1500 meters. Refer to the national military standards (such as GJB1172 and GJB3617, etc.) for the range criteria of air pressure and temperature, and set the extreme value range for the three parameters of air pressure, air temperature and temperature of the low-altitude sounding rocket. See Table 1. Element range table.

[0031]

[0032] Table 1

[0033] In the process of observation data processing, there are three sensors (pressure sensor, temperature sensor and humidity sensor) data in each observation layer, so the observation data of a certain sensor in a certain observation layer may be abnormal, while the observation data of other sensors are normal. If all the observation data of this layer is deleted, then deleting the data of this layer will inevitably cause the normal observation data to be deleted. Therefore, in this case, the deletion...

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Abstract

The invention relates to a sea data processing realization method based on a low-altitude sounding rocket. The method comprises the following steps: a data scope is limited, a landing phase point of the sounding rocket is extracted, the landing phase point of the sounding rocket is determined, according to phenomenon of linear change of air pressure at a vertical direction with height, a highest point of the rocket is a lowest point of the air pressure, an air pressure gradient detection method is employed to determine a start point of the decrease phase, and the landing phase data is extracted; and an observation data stabilization point of the landing phase is continuously determined; the data is subjected to Rendal error control, whether a certain essential factor sequence in the observation data is in a reasonable value range is determined, a moving average method is used for filtering the essential factor to obtain a novel essential factor sequence, by comparing a relation betweena mean square deviation K of the corresponding essential factors before and after filtering and m times of mean square deviation, exception handling is carried out on the observation data, and an interpolation is used for substituting an abnormal value. The method can increase the quality of the sea data.

Description

technical field [0001] The invention belongs to the field of data processing, and relates to a data processing method for ocean data detection equipment—low-altitude sounding rockets. Background technique [0002] At present, the demand for marine environment informatization is increasing, and the new generation of marine survey equipment has the characteristics of high observation accuracy, short sampling interval, large amount of information, and easy use. Among them, the low-altitude sounding rocket is a sounding device used to detect the environmental parameters of the ocean-atmospheric boundary layer and the mixed layer. The sensors carried on the sounding instrument can detect atmospheric environmental parameters such as temperature, air pressure, and relative humidity. Low-altitude sounding rockets are usually launched on ships. The rocket launch altitude is about 1,000 meters. After passing the highest point, the parachute opens and sends data stably, once every seco...

Claims

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Application Information

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IPC IPC(8): G01C13/00G06F17/18
CPCG01C13/00G06F17/18
Inventor 杨嘉琛王畅
Owner TIANJIN UNIV
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