| 摘要 |
FIELD: weapons and ammunition.SUBSTANCE: sight incorporates transducer of angles and two-axis bore sight angular speed transducer. Launch permit signal generator is connected to said transducers as well as bore sight angular position indicator. Launcher incorporates rocket availability pickup. Rocket guidance device is connected to bore sight angle transducers in first version, and, in second version, to transducer of angles and two-axis bore sight angular speed transducer. In compliance with third version, it is connected to rocket launch permit signal generator. Integral lunch permit signal generator unit inputs are connected to launch permit signal generator, rocket availability pickup and rocket guidance device. "LAUNCH" signal switch and rocket launch signal generator are connected in series. Second input of the latter is connected to output of integral lunch permit signal generator unit. Rocket launch permit indicator is connected to rocket launch integral permit signal generator. Rocket guidance device may be connected additionally to either "LAUNCH" signal switch or rocket availability pickup.EFFECT: higher accuracy of fire.9 cl, 9 dwg |
