首页> 外国专利> METHOD OF GENERATING CONTROL INSTRUCTIONS FOR ROCKET ANGLE OF BANK, ROCKET CONTROL SYSTEM, METHOD OF CONVERTING IMPULSES OF ROCKET ROTATING ALONG ITS ANGLE OF BANK AND SINE-COSINE CONVERTER OF ROCKET CONTROL SYSTEM

METHOD OF GENERATING CONTROL INSTRUCTIONS FOR ROCKET ANGLE OF BANK, ROCKET CONTROL SYSTEM, METHOD OF CONVERTING IMPULSES OF ROCKET ROTATING ALONG ITS ANGLE OF BANK AND SINE-COSINE CONVERTER OF ROCKET CONTROL SYSTEM

机译:银行火箭角产生控制指令的方法,火箭控制系统,转换火箭在银行角范围内的冲动的方法以及火箭正弦余弦变换器

摘要

FIELD: weapons and ammunition.;SUBSTANCE: method of generating control instructions for rocket rotating along its angle of bank comprises measuring the rocket speed of rotation along angle of bank and integrating it in time, shaping the setting pulses when the integrated signal amplitude reaches preset value. The setting pulses are used to generate switching signals to convert decoded signals into rocket course and pitch control instructions representing a multi-stage approximation of sine and cosine curves with amplitudes corresponding to appropriate decoded signals values and with pulse-repetition cycle equal to the cycle rocket rotation along angle of bank. The control system of aforesaid rocket additionally comprises an angular speed pickup, resetting device, angular interval setting circuit, released integrator and sine-cosine converter. The invention covers also the method of converting pulses to convert coordinates at the rocket control hardware comprising generation of an additional switching pulsed signal that generates, from the second input signal, the 16th approximation of cosine signal. Note here that the decoded course and pitch signals are used as the first and second input signals, while the bank pulses with pulse-repetition cycle equal to 1/16 of the rocket period of rotation with respect to angle of bank are used as pulses. The sine-cosine converter comprises additionally the thirst "exclusive OR" circuit and the second multiplier.;EFFECT: higher accuracy of control signal generation.;4 cl, 3 dwg
机译:领域:武器和弹药。实质:生成用于火箭沿倾斜角旋转的控制指令的方法,包括测量火箭沿倾斜角旋转的速度并及时积分,在积分信号幅度达到预设值时整形设置脉冲值。设置脉冲用于生成切换信号,以将解码信号转换为火箭航向和俯仰控制指令,这些指令表示正弦和余弦曲线的多级逼近,其幅度对应于适当的解码信号值,并且脉冲重复周期等于火箭的周期沿倾斜角旋转。上述火箭的控制系统还包括角速度传感器,复位装置,角间隔设定电路,释放积分器和正弦-余弦转换器。本发明还涵盖了在火箭控制硬件处转换脉冲以转换坐标的方法,该方法包括生成另外的切换脉冲信号,该信号从第二输入信号生成余弦信号的第16 近似值。这里注意,解码的航向和俯仰信号被用作第一和第二输入信号,而脉冲重复周期相对于倾斜角等于火箭旋转周期的1/16的倾斜脉冲被用作脉冲。正弦余弦转换器还包括第三个“异或”电路和第二个乘法器。效果:更高的控制信号生成精度; 4 cl,3 dwg

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