首页> 外国专利> METHOD OF FORMING commands to the rocket, rotate angle of heel missile guidance system, means the transformation of coordinates on the missiles to rotate an angle of heel and sine-cosine transformer

METHOD OF FORMING commands to the rocket, rotate angle of heel missile guidance system, means the transformation of coordinates on the missiles to rotate an angle of heel and sine-cosine transformer

机译:形成火箭指令的方法,后跟导弹制导系统的旋转角度,意味着在导弹上变换坐标以旋转后跟角度和正弦-余弦变换器

摘要

1.method u0444u043eu0440u043cu0438u0440u043eu0432u0430u043du0438u00a0 teams u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 rocket, u0432u0440u0430u0449u0430u044eu0449u0435u0439u0441u00a0 on the corner turn, in which the u0434u0435u043au043eu0434u0438u0440u0443u044eu0442 the signals, with the subsequent production of them team up u0440u0430u0432u043bu0435u043du0438u00a0 rocket ahead and u0442u0430u043du0433u0430u0436u0443, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0, u0438u0437u043cu0435u0440u00a0u044eu0442 and integrate in time (ti) speed u0432u0440u0430u0449u0435u043du0438u00a0 missiles on the corner of list (i), reaching values of r u0430u0437u043cu0430u0445u0430 integrated signal equal to the specified valueby creating pulses, with each pulse of which set the integrator to the u0441u043eu0441u0442u043eu00a0u043du0438u0435 and then re integrate current the value of i, which impulses produce u043au043eu043cu043cu0443u0442u0438u0440u0443u044eu0449u0438u0435 signalswhich is u0434u0435u043au043eu0434u0438u0440u043eu0432u0430u043du043du044bu0435 signals in a team u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 course and u0442u0430u043du0433u0430u0436u0443 as multistage approximation u0441u0438u043du0443u0441u043eu0438u0434u044b and u043au043eu0441u0438u043du0443u0441u043eu0438u0434u044b with ila u043bu0438u0442u0443u0434u0430u043cu0438, respective values u0434u0435u043au043eu0434u0438u0440u043eu0432u0430u043du043du044bu0445 signals and a period equal to the period u043fu043eu0432u0442u043eu0440u0435u043du0438u00a0, u0432u0440u0430u0449u0435u043du0438u00a0 missiles on the list.;2.the system u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 rocket, u0432u0440u0430u0449u0430u044eu0449u0435u0439u0441u00a0 on the corner turn, u0441u043eu0434u0435u0440u0436u0430u0449u0430u00a0 steering transmission consistently included radio and equipment u0440u0430u0437u0434u0435u043bu0435u043du0438u00a0 channels and u0434u0435u043au043eu0434u0438u0440u043e u0432u0430u043du0438u00a0 ahead and u0442u0430u043du0433u0430u0436u0443, u043eu0442u043bu0438u0447u0430u044eu0449u0430u00a0u0441u00a0 because it introduced sensor of angular velocity, the device installed in the u0441u043eu0441u0442u043eu00a0u043du0438u0435, u0437u0430u0434u0430u0442u0447u0438u043a angular interval, u0441u0431u0440u0430 u0441u044bu0432u0430u0435u043cu044bu0439 integrator and sine u043au043eu0441u0438u043du0443u0441u043du044bu0439 converter.in this way the angular velocity sensor is connected with the u0438u043du0442u0435u0433u0440u0438u0440u0443u044eu0449u0438u043c entrance drop integrator, asking the entrance which is connected to the u0437u0430u0434u0430u0442u0447u0438u043au0443 of u0438u043du0442u0435u0440u0432 ala, the device installed in the u0441u043eu0441u0442u043eu00a0u043du0438u0435 connected with the entrance of installation in the u0441u043eu0441u0442u043eu00a0u043du0438u0435 drop integrator and sine u043au043eu0441u0438u043du0443u0441u043du043eu0433u043e u043fu0440u0435u043eu0431u0440u0430u0437u043eu0432u0430u0442u0435u043b u00a0, u0441u0447u0435u0442u043du044bu0439 entrance which is connected with the integrator output drop.the exits of the channels and u0440u0430u0437u0434u0435u043bu0435u043du0438u00a0 u0434u0435u043au043eu0434u0438u0440u043eu0432u0430u043du0438u00a0 ahead and u0442u0430u043du0433u0430u0436u0443 connected respectively with the exchange and u0442u0430u043du0433u0430u0436u043du044bu043c inputs sine u043au043eu0441u0438u043du0443u0441u043du043eu0433u043e u043fu0440u0435u043eu0431u0440u0430u0437u043eu0432u0430u0442u0435 u043bu00a0, first and second outputs of which are connected respectively with the first and second inputs transmission.;3.method u043fu0440u0435u043eu0431u0440u0430u0437u043eu0432u0430u043du0438u00a0 coordinates on a u0432u0440u0430u0449u0430u044eu0449u0435u0439u0441u00a0 on the list, which is the number of pulses and the form of a binary number, u0438u0437u043cu0435u043du00a0u0435u043cu043eu0435 0 d. about 15, which produce u043au043eu043cu043cu0443u0442u0438u0440u0443u044eu0449u0438u0435 pulse signals, a signal 16 step approximation of the input sinusoidal signal, divided, u043eu0442u043bu0438u0447u0430u044eu0449u0438 u0439u0441u00a0 that produce additional selectivity pulse signalwhich one of the second input signal forms a 16 step approximation u043au043eu0441u0438u043du0443u0441u043eu0438u0434u0430u043bu044cu043du043eu0433u043e signal, with a first and second input signals ex u043eu043bu044cu0437u0443u044eu0442 u0434u0435u043au043eu0434u0438u0440u043eu0432u0430u043du043du044bu0435 signals respectively on the rate and u0442u0430u043du0433u0430u0436u0443, as well as the pulses are u043au0440u0435u043du043eu0432u044bu0435 pulse period u043fu043eu0432u0442u043eu0440u0435u043du0438u00a0 which equals to 1 / 16 u0432u0440u0430u0449u0435u043du0438u00a0 period the missiles on the list.;4.sine u043au043eu0441u0438u043du0443u0441u043du044bu0439 converter containing the first u043fu0435u0440u0435u043cu043du043eu0436u0438u0442u0435u043bu044c and meter pulses, the first and third walls which are connected with the first and second inputs of the "logical" exclusive or ", and the second and third outputs from the first and second inputs the second logical" exclusive or ".with the first and second circuits "exclusive or" connected respectively with the first and second inputs the first u043fu0435u0440u0435u043cu043du043eu0436u0438u0442u0435u043bu00a0, the third gate which is connected to the h u0435u0442u0432u0435u0440u0442u044bu043c post meter pulses, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 because it introduced u0442u0440u0435u0442u044cu00a0 u043bu043eu0433u0438u0447u0435u0441u043au0430u00a0 scheme "exclusive or" and the second u043fu0435u0440u0435u043cu043du043eu0436u0438u0442u0435u043bu044c,the first and second inlet which are connected with the outputs first and second logic circuits "exclusive or", with the third and fourth meter pulses of light. combined respectively with the first and second inputs the third logical "exclusive or", which is connected with the third entrance exit the second u043fu0435u0440u0435u043cu043du043eu0436u0438u0442u0435u043bu00a0,with the entrance of sine u043au043eu0441u0438u043du0443u0441u043du043eu0433u043e u043fu0440u0435u043eu0431u0440u0430u0437u043eu0432u0430u0442u0435u043bu00a0 u00a0u0432u043bu00a0u044eu0442u0441u00a0 door installation in the u0441u043eu0441u0442u043eu00a0u043du0438u0435 meter pulses, u043fu043eu0434u0441u043eu0435u0434u0438u043du00a0u0435u043cu044bu0439 out device installation in the u0441u043eu0441u0442u043eu00a0u043du0438u0435, u0441u0447u0435u0442u043du044bu0439 entrance meter pulses, u0441u043eu0435u0434u0438u043du00a0u0435u043cu044bu0439 an integrator gains entrance drop, first u043fu0435u0440u0435u043cu043du043eu0436u0438u0442u0435u043bu00a0 and u0442u0430u043du0433u0430u0436u043du044bu0439 entrance wto whom u043fu0435u0440u0435u043cu043du043eu0436u0438u0442u0435u043bu00a0,u0441u043eu0435u0434u0438u043du00a0u0435u043cu044bu0435 respectively with the outputs of u0440u0430u0437u0434u0435u043bu0435u043du0438u00a0 channels and u0434u0435u043au043eu0434u0438u0440u043eu0432u0430u043du0438u00a0 and outputs sine u043au043eu0441u0438u043du0443u0441u043du043eu0433u043e u043fu0440u0435u043eu0431u0440u0430u0437u043eu0432u0430u0442u0435u043bu00a0 - exits the first and second per u0435u043cu043du043eu0436u0438u0442u0435u043bu0435u0439, u0441u043eu0435u0434u0438u043du00a0u0435u043cu044bu0435 with first and second inputs transmission.
机译:1.方法 u0444 u043e u0440 u043c u0438 u0440 u043e u0432 u0430 u043d u0438 u00a0球队 u0443 u043f u0440 u0430 u0432 u043b u0435 u043d u0438 u00a0火箭, u0432 u0440 u0430 u0449 u0430 u044e u0449 u0435 u0439 u0441 u00a0在拐角处,其中 u0434 u0435 u043a u043e u0434 u0438 u0440 u0443 u044e u0442信号,并随后产生信号,将 u0440 u0430 u0432 u043b u0435 u043d u0438 u00a0火箭向前,并将 u0442 u0430 u043d u0433 u0430 u0436 u0443, u043e u0442 u043b u0438 u0447 u0430 u044e u0449 u0438 u0439 u0441 u00a0, u0438 u0437 u043c u0435 u0440 u00a0 u044e u0442并以时间(ti)速度 u0432 u0440 u0430进行积分清单(i)角上的 u0449 u0435 u043d u0438 u00a0导弹,通过创建脉冲,使r u0430 u0437 u043c u0430 u0445 u0430积分信号的值等于指定值,每个脉冲将积分器设置为 u0441 u043e u0441 u0442 u043e u00a0 u043d u0438 u0435,然后将当前值o重新积分fi,这些脉冲会产生 u043a u043e u043c u043c u0443 u0442 u0438 u0440 u0443 u044e u0449 u0438 u0435信号,即 u0434 u0435 u043a u043a u043e u0434 u0438 u0440 u043e u0432 u0430 u043d u043d u044b u0435在团队中发信号 u0443 u043f u0440 u0430 u0432 u043b u0435 u043d u043d u0438 u00a0课程和 u0442 u0430 u043d u043d u0433 u0430 u04436 u0443作为多级逼近 u0441 u0438 u043d u0443 u0441 u043e u0438 u0434 u0434 u044b和 u043a u043e u0441 u0441 u0438 u043d u0443 u0441 u0431 u043e u043e u0438 u0434 u044b u0438 u0442 u0443 u0434 u0430 u043c u0438,各自的值 u0434 u0435 u043a u043e u0434 u0438 u0440 u043e u0432 u0430 u043d u043d u043d u044b u0445清单上的时期为 u043f u043e u0432 u0442 u043e u0440 u0435 u043d u04438 u0449 u00a0, u0432 u0440 u0430 u0449 u0435 u043d u0438 u00a0上的导弹; 2.系统u0443 u043f u0440 u0430 u0432 u043b u0435 u043d u0438 u00a0火箭, u0432 u0440 u0430 u0449 u0430 u044e u0449 u0435 u0435 u0439 u0441 u00a0 u0441 u043e u0434 u0435 u0440 u0436 u0430 u0449 u0430 u00a0始终包括无线电和设备 u0440 u0430 u0437 u0434 u0435 u043b u0435 u043d u043d u0438 u00a0频道和 u0434 u0435 u043a u043e u0434 u0438 u0440 u043e u0432 u0430 u043d u0438 u00a0前面和 u0442 u0430 u043d u0433 u0430 u0436 u0443, u043e u0442 u043b u043b u0447 u0430 u044e u0449 u0430 u00a0 u0441 u00a0,因为它引入了角速度传感器,因此该设备安装在 u0441 u043e u0441 u0442 u043e u00a0 u043d u0438 u0435, u0437 u0430 u0434 u0430 u0442 u0447 u0438 u043a角度间隔, u0441 u0431 u0440 u0430 u0441 u044b u0432 u0430 u0435 u043c u044b u0439积分器和正弦 u043a u043e 044 u0438 u043d u0443 u0441 u043d u044b u0439转换器。这样,角速度传感器与 u0438 u043d u0442 u0435 u0433 u0440 u0438 u0440 u0443 u044e u0449 u0438 u043c入口下落积分器,询问与 u0437 u0430 u0连接的入口 u0438 u043d u0442 u0435 u0440 u0432 ala的434 u0430 u0442 u0447 u0438 u043a u0443,安装在 u0441 u043e u0441 u0442 u0432 u043e u00a0 u043d u0438 u0435与 u0441 u043e u0441 u0442 u043e u00a0 u043d u0438 u0435下降积分器和正弦 u043a u043e u0441 u0438 u043d u043d u0433 u0441 u043d u043e u0433 u043e u043f u0440 u0435 u043e u0431 u0440 u0430 u0437 u043e u0432 u0430 u0442 u0435 u043b u00a0, u0441 u0447 u0435 u0442 u043d u044b u0439通道出口和 u0440 u0430 u0437 u0434 u0435 u0435 u043b u0435 u043d u0438 u00a0 u0434 u0435 u043a u043e u043e u043e u043e u043e u0434 u0434 u0440 u043e u0432 u0430 u043d u0438 u00a0前面和 u0442 u0430 u043d u0433 u0430 u0436 u0443分别与交换机相连,并且 u0442 u0430 u043d u0433 u0430 u0430 u0436 u043d u044b u043c输入正弦 u043a u043e u0441 u0438 u043d u0443 u0441 u043d u043e u0433 u043e u043f u0440 u0435 u043e u0431 u0440 u0430 u0437 u043e u0432 u0430 u0442 u0435 u043b u00a0,其第一输出和第二输出分别与第一输入和第二输入传输相连。3。方法 u043f u0440 u0435 u043e u0431 u0440 u0430 u0437 u043e u0432 u0430 u043d u0438 u00a0在清单上的 u0432 u0440 u0430 u0449 u0430 u044e u0449 u0435 u0439 u0441 u00a0坐标上脉冲数和二进制数形式 u0438 u0437 u043c u0435 u043d u00a0 u0435 u043c u043e u0435 0 d。大约15个,产生 u043a u043e u043c u043c u0443 u0442 u0438 u0440 u0443 u044e u0449 u0438 u0435脉冲信号,输入正弦信号的信号近似16步,除以 u043e u0442 u043b u0438 u0447 u0430 u044e u0449 u0438 u0439 u0441 u00a0会产生附加的选择性脉冲信号,第二个输入信号之一形成一个16阶逼近 u043a u043e u0441 u0441 u0438 u043d u0443 u0441 u043e u0438 u0434 u0430 u043b u044c u043d u043e u0433 u043e信号,具有第一和第二输入信号,例如 u043e u043b u044c u0437 u0443 u044e u0442 u0434 u0435 u043a u043e u0434 u0438 u0440 u043e u0432 u0430 u0430 u043d u043d u044b u0435分别以速率和 u0442 u0430 u043d u0433 u0430 u0436 u0443发出信号,脉冲为 u043a u0440 u0435 u043d u043e u0432 u044b u0435脉冲周期 u043f u043e u0432 u0442 u043e u0440 u0435 u043d u0438 u00a0等于1 / 16 u0432 u0440 u0430 u0449 u0435 u043d u0438 u00a0对清单中的导弹进行计时; 4.正弦 u043a u043e u0441 u0438 u043d u0443 u0441 u043d u044b u0439转换器包含第一个 u043f u0435 u0440 u0435 u043c u043d u043e u0436 u0438 u0442 u0435 u043b u044c和计量脉冲,第一和第三壁与“逻辑”异或的第一和第二输入相连,第一和第二输入的第二和第三输出与逻辑“异”或第二输入相连。第一电路和第二电路“异或”分别与第一个和第二个输入第一个 u043f u0435 u0440 u0435 u043c u043d u043e u0436 u0438 u0442 u0435 u043b u00a0,第三个门连接到h u0435 u0442 u0432 u0435 u0440 u0442 u044b u043c后计量脉冲, u043e u0442 u043b u0438 u0447 u0430 u044e u0449 u0438 u0439 u0441 u00a0是因为它引入了 u0442 u0440 u0435 u0442 u044c u00a0 u043b u043e u0433 u0438 u0447 u0435 u0441 u043a u0430 u00a0方案“ exclusive or ”和第二个 u043f u0435 u0440 u0435 u0435 u043c u043d u043e u0436 u0438第一和第二入口与第一和第二逻辑电路“异或”连接,并具有第三和第四米光脉冲。分别与第一个输入和第二个输入相结合的第三个逻辑“异或”,与第三个入口出口相连的第二个逻辑“ u043f u0435 u0440 u0435 u043c u043d u043e u0436 u0438 u0442 u043b u00a0,正弦的入口 u043a u043e u0441 u0438 u043d u0443 u0441 u043d u043e u0433 u043e u043f u0440 u0435 u0435 u043e u0431 u0440 u0430 u0435 u0435 u043e u0431 u0440 u0432 u0430 u0442 u0435 u043b u00a0 u00a0 u0432 u043b u00a0 u044e u0442 u0441 u00a0门安装在 u0441 u043e u0441 u0442 u0432 u043e u00a0 u043d u0仪表脉冲, u043f u043e u0434 u0441 u043e u0435 u0434 u0438 u043d u00a0 u0435 u043c u044b u0439将设备安装到 u0441 u043e u0441 u0441 u0442 u043e u00a0 u043d u0438 u0435, u0441 u0447 u0435 u0442 u043d u044b u0439入口仪表脉冲, u0441 u043e u0435 u0434 u0434 u0438 u043d u00a0 u0435 u0435 u043c u044b u0439 ,第一个 u043f u0435 u0440 u0435 u043c u043d u043e u0436 u0438 u0442 u0435 u043b u00a0和 u0442 u0430 u0 43d u0433 u0430 u0436 u043d u044b u0439入场人 u043f u0435 u0440 u0435 u043c u043d u043e u0436 u0438 u0442 u0435 u0435 u043b u00a0, u0441 u043e u043e u0435 u0434 u0438 u043d u00a0 u0435 u043c u044b u0435的输出分别为 u0440 u0430 u0437 u0434 u0435 u043b u0435 u043d u0438 u00a0通道和 u0434 u0435 u043a u043e u0434 u0438 u0440 u043e u0432 u0430 u043d u0438 u00a0并输出正弦 u043a u043e u0441 u0438 u043d u0443 u0441 u043d u043e u0433 u043e u043f u0440 u043e u043e u0431 u0440 u0430 u0437 u043e u0432 u0430 u0442 u0435 u043b u00b0-退出每个 u0435 u043c u043d u043e u0436 u0438 u0442 u0435 u043b u0435 u0439, u0441 u043e u0435 u0434 u0438 u043d u00a0 u0435 u043c u044b u0435具有第一和第二输入传输。

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