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A method of testing the developed torque steering gear Electro-guided missiles and shells
A method of testing the developed torque steering gear Electro-guided missiles and shells
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机译:一种测试已开发的扭矩舵机电导导弹和炮弹的方法
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摘要
method of checking the u044du043bu0435u043au0442u0440u043eu043fu043du0435u0432u043cu0430u0442u0438u0447u0435u0441u043au043eu0433u043e available transmission u0443u043fu0440u0430u0432u043bu00a0u0435u043cu044bu0445 missiles and u0441u043du0430u0440u00a0u0434u043eu0432, based on the measurement of u0432u0440u0430u0449u0430u044eu0449u0435u0433u043e moment actuator with the help of the reference load and u043bu0435u0433u043au043eu0441u044au0435u043cu043du043eu0433u043e u043du0430u0434u0435u0432u0430u0435u043cu043eu0433u043e balanced lever on the steering wheel, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0, set on the installation table steering transmission sensor u043fu0435u0440u0435u043cu0435u0449u0435u043du0438u00a0 controls.met in a separate contact or touch sensor or use u0438u043cu0435u044eu0449u0438u0439u0441u00a0 actuator as a sensor feedback u0441u0432u00a0u0437u0438 sensor linear p u0435u0440u0435u043cu0435u0449u0435u043du0438u00a0 u043fu043eu0440u0448u043du00a0 or angular u043fu0435u0440u0435u043cu0435u0449u0435u043du0438u00a0 controls.turn the wheel to the maximum angle + max in one direction by u043fu0440u0438u043bu043eu0436u0435u043du0438u00a0 u0432u0440u0430u0449u0430u044eu0449u0435u0433u043e since a label dfid = Ql1cosmax reference load q on the u043eu043fu0440u0435u0434u0435u043b weight u0435u043du043du043eu0439 length l1 shoulder u0440u0430u0437u043cu0435u0449u0435u043du0438u00a0 cargo on the lever on the u0432u0440u0430u0449u0435u043du0438u00a0 controls, equal u0440u0430u0437u0432u0438u0432u0430u0435u043cu043eu043cu0443 transmission for a given time u0440u0437u0430u0434 pressure u043fu0438u0442u0430u043du0438u00a0 include power sensoruse a voltmeter and u0438u0437u043cu0435u0440u00a0u044eu0442 u043du0430u043fu0440u00a0u0436u0435u043du0438u0435 u1 at the output of the sensor in torque u0441u043du00a0u0442u0438u0435u043c reference load, turning on the planes, the maximum angle is the maximum in the other parties at the moment by u043fu0440u0438u043bu043eu0436u0435u043du0438u00a0 u0432u0440u0430u0449u0430u044eu0449u0435u0433u043e u043cu043du0432u0440u043fu0440u043eu0442u0438u0432u043eu043fu043eu043bu043eu0436u043du043eu0433u043e mark equal to the maximum load at the time u043cmaxu0448u0448u0430u0440u043du0438u0440u043du043eu0439 u0440u0443u043bu00a0u0445 from steering angle controls and angle at aki missiles, u0441u043du0430u0440u00a0u0434u0430,the power supply u0443u0441u0438u043bu0438u0442u0435u043bu00a0 include transmission and serves for the transmission, compressed air pressure (p = 1,5u0440u0437u0430u0434, serves to the maximum signal transmission u0443u043fu0440u0430u0432u043bu0435u043du0438;u + i, the displacement controls the maximum angle + max u0438u0437u043cu0435u0440u00a0u044eu0442 u043du0430u043fu0440u00a0u0436u0435u043du0438u0435 u2 at the output of the sensor, which should u0443u0434u043eu0432u043bu0435u0442u0432u043eu0440u00a0u0442u044c ratio;U2U1,;through the smooth u0441u043du0438u0436u0435u043du0438u00a0 u0434u0430u0432u043bu0435u043du0438u00a0 u043fu0438u0442u0430u043du0438u00a0 in u043fu043du0435u0432u043cu043eu0441u0435u0442u0438 transmission to reduce the u043du0430u043fu0440u00a0u0436u0435u043du0438u00a0 outlet pressure sensor u043eu043fu0440u0435u0434u0435u043bu00a0u044eu0442 r + 1, which is u043du0430u043fu0440u00a0u0436u0435u043du0438u0435 ud u043eu0432u043bu0435u0442u0432u043eu0440u00a0u0442u044c ratio;u3 = (0.98 - 0.05) u1, the pressure p + 1u0434u043eu043bu0436u043du043e be not more than u0440u0437u0430u0434, making u043fu043du0435u0432u043cu043eu043fu0438u0442u0430u043du0438u0435 and supply u0443u0441u0438u043bu0438u0442u0435u043bu00a0 drive and turns off the signal u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 u + wah food dutch ica, followed in the same manner u0438u0437u043cu0435u0440u00a0u044eu0442 u043du0430u043fu0440u00a0u0436u0435u043du0438u00a0 u1, u2, u3 and u043eu043fu0440u0435u0434u0435u043bu00a0u044eu0442 pressure p at the annex relevant points and signal u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 u - u0443u043fu0440u043eu0442u0438u0432u043eu043fu043e the error signal and u043eu043fu0440u0435u0434u0435u043bu00a0u044eu0442 u0440u0430u0437u0432u0438u0432u0430u0435u043cu044bu0439 moment u043cu0440u0430u0437u0432,transmission formula;Mu0440u0430u0437u0432 = kp + (-) 1SnRcosmax,;where the sn - u044du0444u0444u0435u043au0442u0438u0432u043du0430u00a0 square u043fu043eu0440u0448u043du00a0 of u043fu043du0435u0432u043cu043eu0446u0438u043bu0438u043du0434u0440u0430 drive;;r is a parameter u043fu0440u0435u043eu0431u0440u0430u0437u043eu0432u0430u043du0438u00a0 sustained u0434u0432u0438u0436u0435u043du0438u00a0 u043fu043eu0440u0448u043du00a0 in rotational controls;;p + (-) 1 - u0438u0437u043cu0435u0440u0435u043du043du0430u00a0 value u0434u0430u0432u043bu0435u043du0438u00a0 by rejecting controls transmission to focus in one and the other sides;;the rate of u0438u0441u043fu043eu043bu044cu0437u043eu0432u0430u043du0438u00a0 actuator under pressure, u043eu043fu0440u0435u0434u0435u043bu00a0u0435u043cu044bu0439 type distribution device and u043fu043eu0442u0435u0440u00a0u043cu0438 u0434u0430u0432u043bu0435u043du0438u00a0 actuator to the distribution u0443u0441u0442u0440u043eu0439u0441 twa.
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