Micro gyroscope adaptive control method based on model reference
A technology of adaptive control and micro gyroscope, applied in the field of control system, can solve the problems of the characteristics and design differences of the original components, the bad influence of environmental changes, and the inability to solve the problems of zero angular rate output, etc., to achieve the effect of improving robustness
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Publication Date
- 2013-03-27
- Estimated Expiration
- Not applicable · inactive patent
Smart Images
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Abstract
Description
technical field
[0001] The invention relates to a control method of a gyroscope, in particular to a method for adaptively controlling a micro gyroscope based on a model reference, and belongs to the technical field of control systems. Background technique
[0002] Micro gyroscopes are inertial sensors that measure angular rates. Compared with traditional gyroscopes, micro gyroscopes have huge advantages in size and cost, so they have a broad application market, such as in navigation guidance, consumer electronics, navigation and national defense. . However, due to the existence of errors in the manufacturing process and the influence of the ambient temperature, the difference between the characteristics of the original and the design results in a coupled stiffness coefficient and damping coefficient, which reduces the sensitivity and accuracy of the micro gyroscope. In addition, the gyroscope itself is a multi-input and multi-output system, and there are parameter uncertain...
Examples
Embodiment Construction
[0027] The method for self-adaptive control of a micro-gyroscope based on model reference proposed by the present invention will be described in detail below with reference to the accompanying drawings and embodiments.
[0028] Such as figure 1 , figure 2 , image 3 , Figure 4 , Figure 5 As shown, the method for adaptively controlling a micro-gyroscope based on a model reference in a preferred embodiment of the present invention includes the following steps,
[0029] (1) Establish an ideal kinetic model
[0030] The design reference model is two sine waves of different frequencies with amplitude x m =A 1 sin(w 1 t), y m =A 2 sin(w 2 t), where w 1 ≠w 2 and are not zero, written in state space as:
[0031] (2) Based on the Lyapunov method to control the micro gyroscope
[0032] Using the state vector X and tracking error e of the micro-gyroscope as the input signal of the feedback controller, the design control law is: u=K T x+K f e, where K T Controller pa...