| 摘要 |
An interconnect system between an off-center-line gun of an aircraft and the aircraft rudder control. When the off-center gun is fired, the trigger actuation creates a signal modified by dynamic compressible pressure Qc to cause the interconnect system to automatically deflect the rudder an amount to cancel the yaw moment produced by the gun firing. Circuitry is also disclosed to additionally compensate for any yaw moment which may arise from an extendable gun gas deflector door. The full specification must be consulted for an understanding of the invention.
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