Method, device and electronic equipment for determining aircraft control capability
A technology of control ability and determination method, which is applied in the direction of ground device, control/regulation system, non-electric variable control, etc., can solve the problems of large structure size of control rudder surface, increase the weight of the whole machine and the energy consumption of the steering gear, so as to reduce the overall The effect of reducing the weight of the steering gear and the energy consumption of the steering gear, reducing the demand for control capability, and reducing the size of the structure
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[0108] The specific implementation manners of the present invention will be further described in detail below in conjunction with the drawings and specific embodiments.
[0109] see figure 1 , an embodiment of the present invention provides a method for determining an aircraft control capability, including:
[0110] Step 101: According to the overall parameters, ballistic data and aerodynamic data of the aircraft, calculate the first parameter and the second parameter corresponding to each flight ballistic state point, wherein the first parameter is the coupling influence evaluation parameter of the aileron control on the heading stability , the second parameter is a lateral-direction coupling dynamic heading stability parameter;
[0111] Specifically, the coupling influence evaluation parameter of the aileron control on the heading stability, denoted as ACATD (aileron control affection to direction), can be determined according to the stability of the heading and the steerin...
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