| 摘要 |
The invention relates to the branch of special equipment, in particular to the system of control of attitude and stabilization of aircraft. In a method of forming drive signal for jet engines of orientation of aircraft during its three-dimensional reorientation additionally a drive signal is formed of the value of ratio of program moment of aircraft to the maximum moment taking into account its asymmetry and systematic disturbing moment, which appears due to deviation of the centre of masses of article from its longitudinal axis, and calculated moment, which is created by the engines of stabilization. With the method forming the drive signal of adjustment of systematic disturbances occurs according to the open pattern, and random disturbances – to the closed pattern. The invention provides for increase of accuracy of fulfilment of the aircraft reorientation, decrease of energy consumption, reduction of relaxation time of the object of control upon termination of angular manoeuvre. |
