Flight path control system
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12. IN AN ARTIFICIAL FEEL SYSTEM FOR CONTROLLING AN AIRCRAFT ABOUT AN AXIS, A SERVOMOTOR HAVING A DIFFERENTIAL CONTROL LINK WITH A FIRST INPUT OPERABLE TO MOVE THE CRAFT ABOUT ITS AXIS AND A SECOND INPUT OPERABLE TO DAMP THE SYSTEM, A MANUAL CONTROL MEMBER, MEANS PROVIDING THE FIRST INPUT TO THE LINK INCLUDING A FORCE SENSOR AT THE MEMBER PROVIDING A COMMAND SIGNAL DEPENDING ON THE MANUAL FORCE EXERTED ON THE MEMBER, AN ACCELEROMETER PROVIDING A SIGNAL DEPENDING ON THE ANGULAR ACCELERATION OF THE CRAFT ABOUT ITS AXIS, AND MEANS CONNECTED TO SAID LINK TO PROVIDE THE SECOND INPUT TO SAID SERVOMOTOR RESPONSIVE TO
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12 Claims
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12. IN AN ARTIFICIAL FEEL SYSTEM FOR CONTROLLING AN AIRCRAFT ABOUT AN AXIS, A SERVOMOTOR HAVING A DIFFERENTIAL CONTROL LINK WITH A FIRST INPUT OPERABLE TO MOVE THE CRAFT ABOUT ITS AXIS AND A SECOND INPUT OPERABLE TO DAMP THE SYSTEM, A MANUAL CONTROL MEMBER, MEANS PROVIDING THE FIRST INPUT TO THE LINK INCLUDING A FORCE SENSOR AT THE MEMBER PROVIDING A COMMAND SIGNAL DEPENDING ON THE MANUAL FORCE EXERTED ON THE MEMBER, AN ACCELEROMETER PROVIDING A SIGNAL DEPENDING ON THE ANGULAR ACCELERATION OF THE CRAFT ABOUT ITS AXIS, AND MEANS CONNECTED TO SAID LINK TO PROVIDE THE SECOND INPUT TO SAID SERVOMOTOR RESPONSIVE TO
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