FIELD: guidance systems.
SUBSTANCE: invention relates to guidance systems for high-speed and maneuvering purposes, in particular to guidance systems for hypersonic aircraft (HSAC). Control system ensures that the target is intercepted with high accuracy, taking into account only cornering errors and angular velocity errors. With the help of the direction finder or other sources of information, a target bearing measurement is formed, on the basis of which the estimations of the required values of the target sight angle and its derivative are formed in the filters, as well as their current values, which are transmitted to amplifiers, where signals are simultaneously generated. Generated signals are transmitted to the adder, in which the interceptor control signal is generated. Signal is transmitted to the interceptor controls, which change its spatial position.
EFFECT: method will provide higher stability and accuracy of interception of high-speed and maneuvering targets, including HSAC.
1 cl, 7 dwg
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