|
ANALYSIS
OF GUIDANCE AND CONTROL SIGNALS DURING FLIGHT TESTS OF AN ANTITANK MISSILE
Kobilarev Miodrag
The procedure of flight tests of a short-distance antitank missile system has been presented. Flight tests by missile launching to a fixed target have been carried out in order to check the missile external-balistic parameters, the guidance and control system as well as other missile functions using highspeed video and TV cameras and the digital acquisition system.
Ključne reči: Guided missile, flight tests, free gyroscope, thrust vector control, signal analysis. |