According to the needs of flight, based on the automatic control technology, the steering gear and the vertical gyroscope are used to realize the sliding approach, free elevation and attitude maintenance, and the structured design of the shoe-type aircraft. The fine adjustment of the rising rudder angle and the different rotation force of the pitch angle can carry out error tracking, realize the stable adjustment of different states, and also achieve the purpose of rapid response. The accuracy of the cooperation between the two boots also depends on the optimization strategy of the system and the control of the rising threshold. The deficiencies in the initial setting model can be adjusted through the advanced filtering and lagging network correction of the model to achieve the precise service of the system And seamless cooperation. This article gives the automatic control design steps and optimized paths for precise adjustment.
Research on Modular Cooperative Optimal Control of Low Altitude Approach Booted Aircraft
2021-10-20
1140621 byte
Conference paper
Electronic Resource
English
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