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Method for controlling control parameters in an air vehicle and system of controlling an air vehicle
Method for controlling control parameters in an air vehicle and system of controlling an air vehicle
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机译:用于控制飞行器中的控制参数的方法和控制飞行器的系统
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摘要
According to the method of the invention, control parameters V indicating speed, R indicating turn characteristics and γ indicating a path angle are determined such that these parameters are maintained between limits, and such that one of them deviates as little as possible from a corresponding control input parameter Ri. In order to maintain (as much as possible) the value of R unchanged, V can be varied. The method may include the calculation of the maximum and minimum thrust available.
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