Full-automatic triaxial air bearing table micro-interference force moment measurement system and method
A technology of micro-disturbance torque and measurement method, applied in the direction of measuring device, torque measurement, power measurement, etc., can solve the problems of limited accuracy of angle measurement rate, long integration time, lack of test data support, etc.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Publication Date
- 2014-12-10
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Abstract
Description
technical field
[0001] The present invention relates to the measurement of micro-level disturbance torque, and more specifically relates to a three-axis air bearing table and the like that need to accurately measure disturbance torque in all directions, and at the same time, there is mechanical interference in single-axis measurement, which makes it difficult to measure. Background technique
[0002] As an effective ground test equipment for the development of high-precision spacecraft and the verification of attitude control systems and compensation algorithms, the three-axis air bearing table needs to accurately measure the disturbance torque in all directions. Current engineering practice is generally based on Measure the longitudinal disturbance moment, but because the disturbance moment T d The magnitude of the gyroscope is very small, and the accuracy of the angle measurement rate of instruments such as gyroscopes is limited. When measuring the disturbance torque by ...
Examples
Embodiment Construction
[0028] Embodiments of the present invention are described in detail below, and the present embodiment is implemented on the premise of the technical solution of the present invention, and detailed implementation and specific operation process are provided, but the protection scope of the present invention is not limited to the following embodiments.
[0029] Such as Figure 1 ~ Figure 2 As shown, the fully automatic three-axis air bearing micro-disturbance torque measurement system provided by the present invention includes an air floating ball 3 and a ball socket 4, and a gyroscope 1 is installed on the air floating ball 3 for measuring angular velocities in three directions ω m , three trim masses m are installed on the air float 3 1 6.m 2 7.m 3 8 and the jet system (not shown in the figure), the moment of inertia matrix of the system formed by the air float 3, the gyroscope 1, three mass blocks and the jet system under the coordinates of the air float is a 3 × 3 matrix I...