FIELD: aviation.
SUBSTANCE: to control the motion of aircraft (AC) pre-flight preparation is carried out by using mathematical model AC, original data about dynamic parameters of AC and anchor points in the form of matrices are formed an in-memory data source control system, program trajectory of AC after anchor points is formed, in the process of flight trajectory of AC is restores by smooth transition between the anchor points, AC motion control is carries out using the proportional navigation method, and dynamic correction of program trajectory in a certain way.
EFFECT: increasing the accuracy and adequacy of the formation of the trajectory during the flight of an aircraft with a reduction in the computational complexity.
1 dwg
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