Method for measuring rotating angle of aircraft based on nuclear magnetic resonance

A technology of rotation angle and measurement method, applied in the direction of steering induction equipment, etc., can solve the problem of large measurement error, and achieve the effect of overcoming measurement error and increasing stability
CN103528580AInactive Publication Date: 2014-01-22INST OF ELECTRICAL ENG CHINESE ACAD OF SCI

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
INST OF ELECTRICAL ENG CHINESE ACAD OF SCI
Publication Date
2014-01-22
Estimated Expiration
Not applicable · inactive patent

Smart Images

  • Figure 1
    Figure 1
  • Figure 2
    Figure 2
Patent Text Reader

Abstract

The invention provides a method for measuring the rotating angle of an aircraft based on nuclear magnetic resonance. The method is characterized in that two isotope nucleuses with the same element and different gyromagnetic ratios serve as a measurement carrier of an aircraft rotating angle measurement gyroscope; an alkali metal element is added into a cylindrical glass sealed cavity in a nuclear magnetic resonance resonant cavity of the aircraft rotating angle measurement gyroscope based on a spin polarization exchange mechanism; electron spin polarization of alkali metal atoms is transferred to two isotopic atoms serving as the rotating speed measurement carrier of the gyroscope to cause net nucleus spin polarization of the two isotopic atoms. Therefore, the magnetic polarization strength of the isotopic measurement carrier can be improved, and a signal to noise ratio of a detected signal can be improved.
Need to check novelty before this filing date? Find Prior Art

Description

technical field

[0001] The invention relates to a measurement method for measuring the spin angle of an aircraft, in particular to a measurement method for a gyroscope for detecting the rotation angle of an aircraft based on the principle of nuclear magnetic resonance. Background technique

[0002] The flight attitude control of aircraft is an important task in inertial navigation. During the flight, the high-speed rotation of the aircraft itself can maintain a stable flight direction. The gyroscope can effectively measure the real-time rotation angle or speed of the object, thus providing important technical parameters for flight navigation control. Traditional gyroscopes, such as mechanical gyroscopes and fiber optic gyroscopes, contain mechanical rotating parts and are very sensitive to motion overload and vibration, which have a certain impact on the design and function of gyroscopes.

[0003] Chinese patent 2006101715882 "Optical fiber gyroscope using low-bias and pol...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More