MISSILES AND CONTROL SYSTEMS THEREFOR
A homing missile of which the target tracker has a restricted, e.g. a slit-shaped, field-of-view and which incorporates means whereby the field-of-view may be rotated, e.g. by rolling the missile, has a control system which to avoid certain instability problems, such as adverse autopilot coupling, i...
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Format: | Patent |
Sprache: | eng ; fre |
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