| 摘要 |
PROBLEM TO BE SOLVED: To control an air frame during reverse and advancement by a single air frame mounted in a missile and having a gain calculator changing over definite dimension differential coefficient, when a speed of a guiding missile moves from a negative to a positive at emission of a missile from the mother airplane, and to simplify the device. SOLUTION: This guided missile separated from a flying airplane, and capable of flying backwardly of the airplane comprises a steering blade for producing aerocontroling force of the air frame; a speed detecting means for detecting a speed of the missile; and the air frame control device for performing gain calculation by switching over definite dimension differential coefficient Zδand Mδbased on the missile speed, thereby simplifying the air frame control device.
|
