| 摘要 |
Guidance system for controlling the flight of a guided missile. This system is characterised in that it comprises an optical device for sighting a target, an manual control device intended to generate first control signals in response to its operation by an operator, means of transmitting the first control signals to a receiver carried by the missile, a tracking device having an optical axis substantially parallel to that of the sight device for generating second trajectory control signals and means of transmitting the second control signals to a receiver of the missile. Guidance of missiles, particularly anti-tank missiles. <IMAGE>
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