FIELD: defense equipment, in particular, complex aids of monitoring of guided missiles.
SUBSTANCE: according to the invention, simulating values of command messages are assigned, they are modulated and converted to an electromagnetic radiation, than is fed to the input of the missile receiving channel, and the missile parameters are checked up. Simultaneously with the assignment of the simulating values of the command messages, a simulating signal of missile rolling is formed, and the signal is applied to the missile roll sensor. The current values of control commands are compared at the missile control actuator with the preliminarily assigned simulating values, and according to the results of the comparison, a conclusion is made on the conformity of the parameters under check with the assigned ones, the frequency of the missile rolling simulating signal is changed in the direct proportion to the missile flight simulating speed, and the missile guidance signal is modulated by a signal simulating the change of the missile attitude relative to the aiming point, in which realization is simplified at a high degree of accuracy of monitoring of the missile parameters. Two modifications of the automatic system of monitoring of the roll-stabilized missile are described.
EFFECT: simplified procedure at an enhanced accuracy.
4 cl, 4 dwg
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