On-line identification system and inertia algorithm for the moment of inertia of a large-scale three-axis air-floating table
A technology of moment of inertia and air bearing table, applied in the field of control, can solve problems such as inability to identify on-line, measurement, and input signal selection method not detailed enough
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Embodiment 1
[0045] like figure 1 — image 3 , An online identification technology for the moment of inertia of a large-scale three-axis air-floating table involved in this embodiment includes: a design scheme of the identification system for the moment of inertia of the three-axis air-floating table and an algorithm derivation for the moment of inertia of the three-axis air-bearing table.
[0046] The design scheme of the moment of inertia identification system of the three-axis air-floating platform, including data processing system 1, display system 2, support and protection system 3, attitude measurement and control system of the three-axis air-floating platform 4, wireless transmission system 5, balance adjustment system 6 and Power supply system 7. The relationship between the above seven systems is as follows: Data processing system 1 performs data processing on the output signal from the on-stage measurement and control system to identify the moment of inertia, display system 2 di...
Embodiment 2
[0048] The derivation of the moment of inertia algorithm of the three-axis air-floating table:
[0049] One algorithm for moment of inertia measurement
[0050] The scheme of identifying the moment of inertia is as follows: use the flywheel as the actuator of the system to input to the air flotation table, measure the angular velocity through the gyroscope as the output of the system, and establish the following dynamic equation:
[0051]
[0052]
[0053] where J f is the moment of inertia of the flywheel, ω f is the rotational speed of the flywheel, J is the moment of inertia of the air-floating table, and ω is the angular velocity of the air-bearing table. In formula (2), since the moment of inertia is large and the attitude control is always performed at a small angle during the identification process, eliminating the small amount in the formula and modifying the position of the input and output can be obtained:
[0054]
[0055] where J -1 is the inverse matrix...
Embodiment 3
[0084] The identification of the moment of inertia of the three-axis air flotation table in this system is a prerequisite for the air flotation table to complete other tasks. Since the three-axis air flotation table needs to be adjusted and balanced before it works, the moment of inertia will change, so as long as the routine The system composed of the three-axis air-floating table has the devices and functions described in this system, and the moment of inertia of the three-axis air-floating table can be identified after other systems complete the required hardware installation and adjustment and balance.
[0085] The system adopts the structure of measurement and control system on the platform, calculation and display control of the host computer system on the platform, wireless communication between the monitoring and control system on the platform and the host computer system on the platform. The off-stage host computer system sends commands, the on-stage measurement and co...
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