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