发明名称 Roll reference for missile guidance - is provided by polarised modulated beam from laser diode directed onto missile
摘要 <p>The anti-aircraft missile is provided with a roll reference in order that corrections to the trajectory may be made. This is provided by an electromagnetic beam with linear polarisation. A laser diode provides a pulsed beam which is polarised and modulated prior to direction onto the missile. A detector(18) on a fin provides a signal representing roll rotation. Another detector(19) provides a normalised signal. The signals are amplified(28, 29) and filtered (68, 69) prior to application to synchronous demodulators (70, 71). Programmable dividers(72, 73) receive the normalised signal(Iii) together with outputs from the demodulator. The resultant signals are applied to a circuit(76) which determines roll angle to k pi radians. Additional circuits(77) determine the value for comparison with a memorised model value(78).</p>
申请公布号 FR2436433(A1) 申请公布日期 1980.04.11
申请号 FR19780026313 申请日期 1978.09.13
申请人 SAGEM 发明人 ALAIN DORE
分类号 F41G7/26;(IPC1-7):05D1/08 主分类号 F41G7/26
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