Helicopter flight control system
First Claim
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12. A HELICOPTER HAVING A ROTOR MEANS COMPRISING:
- MEANS FOR DRIVING SAID ROTOR, MEANS CONNECTED TO SAID DRIVING MEANS FOR CONTROLLING THE ATTITUDE OF THE HELICOPTER ABOUT AN AXIS GENERALLY TRANSVERSE TO THE YAW AXIS OF THE HELICOPTER, MEANS RESPONSIVE TO THE DEVIATION OF THE HELICOPTER IN YAW FROM A PREDETERMINE REFERENCE POSITION FOR PRODUCING A CONTROL SIGNAL REPRESENTATIVE THEREOF,
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12 Claims
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12. A HELICOPTER HAVING A ROTOR MEANS COMPRISING:
- MEANS FOR DRIVING SAID ROTOR, MEANS CONNECTED TO SAID DRIVING MEANS FOR CONTROLLING THE ATTITUDE OF THE HELICOPTER ABOUT AN AXIS GENERALLY TRANSVERSE TO THE YAW AXIS OF THE HELICOPTER, MEANS RESPONSIVE TO THE DEVIATION OF THE HELICOPTER IN YAW FROM A PREDETERMINE REFERENCE POSITION FOR PRODUCING A CONTROL SIGNAL REPRESENTATIVE THEREOF,
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Current AssigneeEverett W. Opdahl, Stanley L. Quick
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Original AssigneeEverett W. Opdahl, Stanley L. Quick
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InventorsQuick, Stanley L., Opdahl, Everett W.
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Application NumberUS04/353,168Time in Patent Office635 DaysField of SearchUS Class Current244/17.13CPC Class CodesB64C 39/022 Tethered aircraft
