![]() SAS2 is the SAS/FPS computer (digital) Three SAS actuators Input Signals: Pitch - rate gyro in the #2 stabilator amplifier Roll - roll rate gyro in the avionics compartment Yaw - yaw rate gyro in the avionics compartmentġ1 SAS 2 Additional Signals #1 & #2 filtered lateral accelerometer Yaw gyro #1 pitch rate gyro #2 vertical gyro #1 lateral accl a/s transducer ![]() SAS1 amplifier (analog) is located in the avionics compartment Three SAS actuators Input Signals: Pitch - rate gyro in the #1 stabilator amplifier Roll - pilot’s (number 2) vertical gyro Yaw - yaw rate gyro in the SAS1 amplifier additional signals - #1 filtered lateral accelerometer, airspeed transducerĩ #1 pitch rate gyro #2 vertical gyro #1 lateral accl a/s transducer SAS systems: SAS 1 & SAS 2 Control Authority: Each SAS has 5% control authority, for a total of 10% Purpose: Provide dynamic stability through short term rate dampening in the pitch, roll, and yaw axis. It is comprised of four subsystems: Stability Augmentation System (SAS) Trim Systems Flight Path Stabilization (FPS) Stabilator (previously discussed)ĥ WHAT IS STABILITY? Create a cool drawing on the dry eraseĦ Stability, in physics and engineering, the property of a body that causes it to return to its original position or motion as a result of the action of the so- called restoring forces, or torques, once the body has been disturbed from a condition of equilibrium or steady motion. Stability Augmentation System TRIM Flight Path Stabilization Malfunction AnalysisĤ WHAT IS AFCS? AFCS enhances the stability and handling qualities of the UH60 helicopter. Instructor Pilot’s understanding of the Automatic Flight Control System NEED: You will be instructing this subject in the near futureģ TOPICS OF DISCUSSION Auto Flight Control System What is Stability? ![]()
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