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Speed measuring method used in rocket sled test

A technology of rocket sled and rocket sled, which is applied in the field of aerospace testing, can solve problems such as the influence of target distance accuracy, instrument erection point error, target distance measurement error, etc., to ensure reliability and continuity, and speed measurement accuracy , high precision effect

Active Publication Date: 2013-09-04
BEIJING INST OF AEROSPACE CONTROL DEVICES
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0009] It can be seen that errors such as installation and debugging errors, distance measurement errors between targets, instrument erection point errors, and dynamic random errors will have a greater impact on the distance accuracy between targets.

Method used

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  • Speed measuring method used in rocket sled test
  • Speed measuring method used in rocket sled test
  • Speed measuring method used in rocket sled test

Examples

Experimental program
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Embodiment Construction

[0027] Two optoelectronic components are installed as figure 2 As shown, the photoelectric components are installed on the side of the rocket sled, and the speed measurement direction of the photoelectric components is parallel to the running direction of the rocket sled, and deviates a certain distance from the orbit. More photoelectric components are installed in the same way, according to the movement direction of the sled, the installation method is presented one after the other, in which the transmitting port and receiving port of each photoelectric component are in a straight line, and the distance between the photoelectric components needs to be accurately measured. Its value is S, and the unit is m. The output signal of the photoelectric component given by the signal receiving end records the time information of the pulse edge through the data recording device, and the time for the blocking signal generated by the same light baffle to the two photoelectric components ...

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Abstract

The invention discloses a speed measuring method used in a rocket sled test. According to the method, two sets of photoelectric assemblies are installed on a sled body in the rocket sled test at an accurate and known interval; when the sled body moves and passes through a light barrier pre-arranged beside a track, a blocking signal is given to the front photoelectric assembly and then a blocking signal is given to the back photoelectric assembly, the two sets of photoelectric assemblies record the time information of the blocking signals respectively through data recording devices, and then the known interval between the two sets of photoelectric assemblies is divided by the time difference between the two blocking signals to obtain the moving speed of the sled body. The speed measuring method used in the rocket sled test is low in cost, short in manufacturing cycle and easy to realize, provides an external measurement method with which the moving speed of the sled body can be measured accurately for the rocket sled test, saves the time for preparing for the test, saves testing expenses, saves labor and materials, and guarantees the reliability and stability of the test.

Description

technical field [0001] The invention relates to a rocket sled test velocity measurement method, in particular to a rocket sled test velocity measurement method based on a 9km track, and belongs to the technical field of aerospace tests. Background technique [0002] The rocket sled is a retrievable test method that uses a rocket engine as power and runs along a specially constructed track. As early as after World War II, in order to promote the development of missile weapons and aerospace, countries such as the United States, Britain, France and the former Soviet Union successively built a variety of different types of test sites, and carried out research and development including inertial measurement devices. Some core components of the rocket skid comprehensive test work. With the development of information warfare and the demand for precise strikes, higher requirements have been put forward for inertial guidance and navigation devices in terms of reliability, practicabil...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F42B35/00F41A31/00
Inventor 魏宗康段宇鹏刘璠刘建波踪华陈东生
Owner BEIJING INST OF AEROSPACE CONTROL DEVICES
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