Vertical/short-range take-off and landing airplane flight control method
A short take-off and landing, flight control technology, applied in the field of flight control, can solve problems such as the influence of the flight control system without considering the dynamic characteristics of the propulsion system, the error of dynamic modeling without consideration, and the disturbance of aircraft attitude
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[0049] The present invention will be further described below in conjunction with the accompanying drawings and examples. The accompanying drawings described here are only used to provide a further understanding of the present invention, which are a part of the application and do not constitute a limitation to the solution of the present invention.
[0050] A flight control method for a vertical / short take-off and landing aircraft, comprising: a transition process controller, a conventional flight mode controller, and a flight mode determiner. The calculation steps of the control algorithm at each time step are as follows:
[0051] (1) Using the measured value y(k) and the state prediction value Calibration status and error estimates { x ^ 1 ( k | k ) , d ^ ( k...
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