FIELD: automatic control systems, applicable in equipment specimens as complex monitoring means, as well as in installations for scientific research work.
SUBSTANCE: simulating instruction in the form of modulated radiation are assigned, the radiation is applied to the input of the missile reception line, and the parameters of the guided missile are estimated by comparison of the signal from the output of the missile control equipment with the preset one. Computation of the three-dimensional motion of the missile is accomplished according to the signals from the output of the missile control equipment, its deviation relative to the aiming point, the modulated radiation is formed in compliance with the obtained deviations of the missile. The monitored parameters are compared with the preset values according to the computed signals of the missile spatial position by comparison of the deviations and the angle of attack and the skip angle or of the missile deviation only with the preset values. The automated system of monitoring of guided missile parameters consists of to series-connected modulated radiation formation unit and the missile control equipment, a computer unit is used, its input is connected to the output of the control equipment, and the output is connected to the input of the modulated radiation formation unit. In the modification of realization of the modulated radiation formation unit it has a series-connected instrument-guidance sight and a controlled mirrors unit optically communicated with the missile control equipment, the second input of the controlled mirrors unit is connected to the outputs of the output of the computer unit.
EFFECT: enhanced truth of the missile parameters monitoring in the conditions of operation of the whole control system, in the presence of disturbing actions and jamming inclusive.
3 cl, 2 dwg
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Authors
Dates
2008-02-10—Published
2006-08-21—Filed